National Library of Energy BETA

Sample records for goddard space flight

  1. Bill Steigerwald Goddard Space Flight Center, Greenbelt, Md.

    E-Print Network [OSTI]

    's Goddard Space Flight Center, the University of Chicago, University of Wisconsin, and the Danish Space will provide a powerful way to tell which of several explanations of the current data are correct. The TopHat experiment includes a spinning telescope and a detector system. It maps a 48-degree diameter disk of the sky

  2. AFFILIATIONS: CAHALAN--NASA Goddard Space Flight Center, Greenbelt, Maryland; OREOPOULOS, VRNAI, AND WEN--University

    E-Print Network [OSTI]

    Robert, Pincus

    M AFFILIATIONS: CAHALAN--NASA Goddard Space Flight Center, Greenbelt, Maryland; OREOPOULOS, VÁRNAI, AND WEN--University of Maryland, Baltimore County, Baltimore, and NASA Goddard Space Flight Center, Greenbelt, Maryland; MARSHAK--NASA Goddard Space Flight Center, Greenbelt, and University of Mary- land

  3. National Aeronautics and Space Administration A Report on the FY 2009 Internal Research and Development Program Goddard Space Flight Center

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration A Report on the FY 2009 Internal Research&D Achievements: #12;About the Cover National Aeronautics and Space Administration Among many other things in FY Aeronautics and Space Administration Goddard Space Flight Center Page 1 http

  4. Cloudy Skies W. Wiscombe and A. Davis NASA Goddard Space Flight Center

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 OutreachProductswsicloudwsiclouddenDVA N C E D BGene NetworkNuclearDNP 20082 P r o jJ. linn Space ScienceW.

  5. GoddardView National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Christian, Eric

    GoddardView National Aeronautics and Space Administration www.nasa.gov Volume 3 Issue 9 July 2007 On Pg 11 National Aeronautics and Space Administration www.nasa.gov Volume 3 Issue 9 July 2007 LRO

  6. GoddardView National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Christian, Eric

    GoddardView National Aeronautics and Space Administration www.nasa.gov Volume 3 Issue 8 June 2007 Commemorative Issue Royal Visit 2007: Her Majesty Queen Elizabeth II May 8, 2007 National Aeronautics and Space

  7. Goddard Space Flight Center Greenbelt, Maryland

    E-Print Network [OSTI]

    linked by microwaves reveal Earth mass in motion -- Ab Davis, GRACE Project Manager, JPL #12;#12;Acknowledgements Content Developed By: Alan Ward Designed By: Winnie Humberson Edited By: Margaret Baguio, Bill, John Ries, Don Chambers,Ab Davis, Mike Watkins. Front Cover Foreground: These images show three

  8. Goddard Space Flight Center Greenbelt, Maryland 20771

    E-Print Network [OSTI]

    pollution can reduce crop yields. Marine plant life depends on iron-rich dust that winds pick up over arid and re-radiate enough heat energy back into the atmosphere to trigger thunderstorms. And because trees. A powerful way to collect such comprehensive data is through the use of satellite sensors that measure

  9. National Aeronautics and Space Administration GoddardViewVolume 5 Issue 6

    E-Print Network [OSTI]

    Christian, Eric

    Goddard ­ 7 A New Mission for Goddard ­ 8 NASA's Solar Dynamics Observatory Arrives at Kennedy Space://internal.gsfc/portal/site/InsideGoddard), hosting an open house for the GLBT community, a panel discussion entitled "Creating an Inclusive Workplace of Housing and Urban Development, the Department of Health and Human Services, the Department of State

  10. National Aeronautics and Space Administration GoddardViewVolume 5 Issue 8

    E-Print Network [OSTI]

    Christian, Eric

    ­ 9 Honey Bees Turned Data Collectors Help Scientists Understand Climate Change ­ 10 Goddard Family Discover will host NASA's climate simulations for the Intergovern- mental Panel on Climate Change. PhotoNational Aeronautics and Space Administration GoddardViewVolume 5 Issue 8 Climate Simulation

  11. NASA/TM2011215870 Goddard's Astrophysics Science Division Annual Report 2010

    E-Print Network [OSTI]

    Christian, Eric

    NASA/TM­2011­215870 Goddard's Astrophysics Science Division Annual Report 2010 Joan Centrella and Francis Reddy, Editors Pat Tyler, Graphical Editor March 2011 NASA Goddard Space Flight Center Greenbelt, Maryland 20771 #12;443 757-5803 443 757-5802 7115 #12;NASA/TM-2011-215870 Goddard's Astrophysics Science

  12. NASA Marshall Space Flight Center Improves Cooling System Performance...

    Office of Environmental Management (EM)

    Marshall Space Flight Center Improves Cooling System Performance NASA Marshall Space Flight Center Improves Cooling System Performance NASA Marshall Space Flight Center Improves...

  13. Seminar 12! The Future of Space Flight!

    E-Print Network [OSTI]

    Stengel, Robert F.

    ! Rationales and Approaches for Human Space Flight! ! Spacecraft Power & Thermal Control! Understanding SpaceSeminar 12! The Future of Space Flight! Spacecraft Power & Thermal Control! Robert Stengel! FRS 112, Sec 13.2, 13.3! 1! 2! #12;3! 4! #12;5! 6! #12;7! 8! #12;Spacecraft Power! 9! Typical Electrical Power

  14. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    . GoddardView Info Goddard View is an official publication of the Goddard Space Flight Center Space Flight Center will be opening its doors to the public for LaunchFest, an open house highlightingNational Aeronautics and Space Administration www.nasa.gov Volume 4, Issue 15 September 2008

  15. National Aeronautics and Space Administration goddardviewVolume 6 Issue 8

    E-Print Network [OSTI]

    Christian, Eric

    GoddardView Info Goddard View is an official publication of the Goddard Space Flight CenterNational Aeronautics and Space Administration goddardviewVolume 6 Issue 8 Fermi Detects `Shocking. It is published bi-weekly by the Office of Public Affairs in the interest of Goddard employees, contractors

  16. NASA/TM-2012-215898 Goddard's Astrophysics Science Division Annual Report 2011

    E-Print Network [OSTI]

    Christian, Eric

    NASA/TM-2012-215898 Goddard's Astrophysics Science Division Annual Report 2011 Joan Centrella and Francis Reddy, Editors Pat Tyler, Graphical Editor May 2012 NASA Goddard Space Flight Center Greenbelt, Maryland 20771 #12;443 757-5803 443 757-5802 7115 #12;NASA/TM-2012

  17. NASA/TM-2013-217509 Goddard's Astrophysics Science Division Annual Report 2012

    E-Print Network [OSTI]

    Christian, Eric

    NASA/TM-2013-217509 Goddard's Astrophysics Science Division Annual Report 2012 Padi Boyd and Francis Reddy, Editors Pat Tyler, Graphical Editor May 2013 NASA Goddard Space Flight Center Greenbelt, Maryland 20771 #12;The NASA STI Program Office ... in Profile Since its founding, NASA has been dedicated

  18. NASA/TM-2014-217523 Goddard's Astrophysics Science Division Annual Report 2013

    E-Print Network [OSTI]

    Christian, Eric

    NASA/TM-2014-217523 Goddard's Astrophysics Science Division Annual Report 2013 Kimberly Weaver and Francis Reddy, Editors Pat Tyler, Graphical Editor June 2014 NASA Goddard Space Flight Center Greenbelt, Maryland 20771 #12;The NASA STI Program Office ... in Profile Since its founding, NASA has been dedicated

  19. National Aeronautics and Space Administration goddardviewVolume 7 Issue 5

    E-Print Network [OSTI]

    Christian, Eric

    include Goddard, the Maryland Department of Natural Resources, the Center for Chesapeake CommunitiesView Info Goddard View is an official publication of the Goddard Space Flight Center. It is published bi miles. These unique ecological resources are among the last sig- nificant tracts of contiguous forest

  20. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    publication of the Goddard Space Flight Center. It is published bi-weekly by the Office of Public AffairsNational Aeronautics and Space Administration www.nasa.gov Volume 2 Issue 5 March 2006 Goddard stories are welcome but will be published as space allows. All submissions are subject to editing. Get

  1. NASA's Marshall Space Flight Center Saves Water with High-Efficiency...

    Office of Environmental Management (EM)

    with High-Efficiency Toilet and Urinal Program NASA Marshall Space Flight Center Improves Cooling System Performance NASA's Marshall Space Flight Center Saves Water with...

  2. Proceedings NASA Goddard Space Flight Center Conference Mass Storage Systems Technologies, September 1719, College Park, MD.

    E-Print Network [OSTI]

    resources required individual applications aggregate demands made by continually increasing number clients users, response time of distributed operations must improve. this paper, analyze measurements Andrew of poor response time significant enough trigger customer dissatisfaction. particular, we show how, after

  3. NASA's Marshall Space Flight Center Improves Cooling System Performanc...

    Broader source: Energy.gov (indexed) [DOE]

    The program saved the facility more than 800,000 gallons of water in eight months. nasa-msfcwatercs2.pdf More Documents & Publications NASA's Marshall Space Flight Center...

  4. NASA's Marshall Space Flight Center Improves Cooling System Performance

    Broader source: Energy.gov [DOE]

    Case study details Marshall Space Flight Center's innovative technologies to improve water efficiency and cooling performance for one of its problematic cooling systems. The program saved the facility more than 800,000 gallons of water in eight months.

  5. Goddard Earth Sciences Data and Information Services Center (GES DISC) http://disc.gsfc.nasa.gov

    E-Print Network [OSTI]

    ://disc.gsfc.nasa.gov NASA Goddard Space Flight Center Code 610.2 Greenbelt, MD 20771 USA README Document for A Multi-Sensor products that now include quality flags. Updated all products with DOI metadata. Gerald Manipon #12;Table

  6. Goddard Scientific Colloquium, May 4, 2012 Aqua at Ten Years and Counting

    E-Print Network [OSTI]

    /Aqua Project Scientist NASA Goddard Space Flight Center #12;Aqua s Delta II Rocket (photos by Bill Ingalls) May Irradiance Monitor (TIM) on the Solar Radiation and Climate Experiment (SORCE) (animation from instrument Data from all 2378 AIRS infrared channels for one footprint off the west coast of South Africa

  7. Flight Projects 2 Technology and Space Program Development 13

    E-Print Network [OSTI]

    are steadily approaching the goal of providing solar cell arrays at a cost com- petitive with other energy#12;Flight Projects 2 Technology and Space Program Development 13 Tracking and Data Acquisition 22, a future in which I feel we will provide unique services to the nation in the exploration of the solar

  8. NASA's Marshall Space Flight Center Improves Cooling System Performance

    SciTech Connect (OSTI)

    2011-02-22

    National Aeronautics and Space Administration’s (NASA) Marshall Space Flight Center (MSFC) has a longstanding sustainability program that revolves around energy and water efficiency as well as environmental protection. MSFC identified a problematic cooling loop with six separate compressor heat exchangers and a history of poor efficiency. The facility engineering team at MSFC partnered with Flozone Services, Incorporated to implement a comprehensive water treatment platform to improve the overall efficiency of the system.

  9. THEMIS Update About Goddard: Goddard Science at the Frontier

    E-Print Network [OSTI]

    Christian, Eric

    of the World's Tiny Pollutants Pg 8 GoddardView National Aeronautics and Space Administration www Philadelphia via "I2" Technology - 7 NASA Probes the Source of the World's Tiny Pollutants - 9 NSPIRES - 10 on Cape Canaveral Air Force Station on Feb. 2 for mating with the Delta II rocket. The Mission Time

  10. The radiation protection problems of high altitude and space flight

    SciTech Connect (OSTI)

    Fry, R.J.M.

    1993-04-01

    This paper considers the radiation environment in aircraft at high altitudes and spacecraft in low earth orbit and in deep space and the factors that influence the dose equivalents. Altitude, latitude and solar cycle are the major influences for flights below the radiation belts. In deep space, solar cycle and the occurrence of solar particle events are the factors of influence. The major radiation effects of concern are cancer and infertility in males. In high altitude aircraft the radiation consists mainly of protons and neutrons, with neutrons contributing about half the equivalent dose. The average dose rate at altitudes of transcontinental flights that approach the polar regions are greater by a factor of about 2.5 than on routes at low latitudes. Current estimates of does to air crews suggest they are well within the ICRP (1990) recommended dose limits for radiation workers.

  11. The radiation protection problems of high altitude and space flight

    SciTech Connect (OSTI)

    Fry, R.J.M.

    1993-01-01

    This paper considers the radiation environment in aircraft at high altitudes and spacecraft in low earth orbit and in deep space and the factors that influence the dose equivalents. Altitude, latitude and solar cycle are the major influences for flights below the radiation belts. In deep space, solar cycle and the occurrence of solar particle events are the factors of influence. The major radiation effects of concern are cancer and infertility in males. In high altitude aircraft the radiation consists mainly of protons and neutrons, with neutrons contributing about half the equivalent dose. The average dose rate at altitudes of transcontinental flights that approach the polar regions are greater by a factor of about 2.5 than on routes at low latitudes. Current estimates of does to air crews suggest they are well within the ICRP (1990) recommended dose limits for radiation workers.

  12. Free space laser communication experiments from Earth to the Lunar Reconnaissance Orbiter in lunar orbit

    E-Print Network [OSTI]

    Sun, Xiaoli

    Laser communication and ranging experiments were successfully conducted from the satellite laser ranging (SLR) station at NASA Goddard Space Flight Center (GSFC) to the Lunar Reconnaissance Orbiter (LRO) in lunar orbit. ...

  13. Model of medical supply demand and astronaut health for long-duration human space flight

    E-Print Network [OSTI]

    Assad, Albert

    2009-01-01

    The medical care of space crews is the primary limiting factor in the achievement of long-duration space missions. (Nicogossian 2003) The goal of this thesis was to develop a model of long-duration human space flight ...

  14. A Compact Nuclear Fusion Reactor for Space Flights

    SciTech Connect (OSTI)

    Nastoyashchiy, Anatoly F. [SRC Troitsk Institute for Innovation and Fusion Research, TRINITI 142190 Troitsk Moscow Reg. (Russian Federation)

    2006-05-02

    A small-scale nuclear fusion reactor is suggested based on the concepts of plasma confinement (with a high pressure gas) which have been patented by the author. The reactor considered can be used as a power setup in space flights. Among the advantages of this reactor is the use of a D3He fuel mixture which at burning gives main reactor products -- charged particles. The energy balance considerably improves, as synchrotron radiation turn out 'captured' in the plasma volume, and dangerous, in the case of classical magnetic confinement, instabilities in the direct current magnetic field configuration proposed do not exist. As a result, the reactor sizes are quite suitable (of the order of several meters). A possibility of making reactive thrust due to employment of ejection of multiply charged ions formed at injection of pellets from some adequate substance into the hot plasma center is considered.

  15. Mikulski and Bolden Visit Goddard

    E-Print Network [OSTI]

    Christian, Eric

    . The recent completion of the critical design review for Webb and the delivery of all its instruments hardware in the Building 29 clean room. Photo credit: NASA/Goddard/Bill Hrybyk Reflecting on Webb Visits Goddard ­ 9 GCDC Science Fair Photo Gallery ­ 10 OutsideGoddard Audrey Haar ­ 12 On the cover

  16. Static Mastermind Wayne Goddard

    E-Print Network [OSTI]

    Goddard, Wayne

    Static Mastermind Wayne Goddard Department of Computer Science University of Natal, Durban Abstract Static mastermind is like normal mastermind, except that the code- breaker must supply at one go a list static mastermind, and calculated the value for a few small cases and provided some upper bounds in a few

  17. Commercial Space Activities at Goddard

    E-Print Network [OSTI]

    Waliser, Duane E.

    Facilities ­ Commercial Payload Partnerships/Rideshares ­ Technology Infusion to Industry · Technology

  18. NASA/TP-2006-214203 Logistics Lessons Learned in NASA Space Flight

    E-Print Network [OSTI]

    de Weck, Olivier L.

    NASA/TP-2006-214203 Logistics Lessons Learned in NASA Space Flight William A. (Andy) Evans, United 2006 #12;NASA STI Program ... in Profile Since its founding, NASA has been dedicated to the advancement of aeronautics and space science. The NASA scientific and technical information (STI) program plays a key part

  19. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 4, Issue 21 December 2008 Goddard and the Virginia Department of Aviation. Established in 1945 by the National Advisory Committee for Aeronautics contributed to both aeronautical and space flight research. The unveiling ceremony included comments by local

  20. Velocity-space sensitivity of the time-of-flight neutron spectrometer at JET

    SciTech Connect (OSTI)

    Jacobsen, A. S. Salewski, M.; Korsholm, S. B.; Leipold, F.; Nielsen, S. K.; Rasmussen, J.; Stejner, M.; Eriksson, J.; Ericsson, G.; Hjalmarsson, A.

    2014-11-15

    The velocity-space sensitivities of fast-ion diagnostics are often described by so-called weight functions. Recently, we formulated weight functions showing the velocity-space sensitivity of the often dominant beam-target part of neutron energy spectra. These weight functions for neutron emission spectrometry (NES) are independent of the particular NES diagnostic. Here we apply these NES weight functions to the time-of-flight spectrometer TOFOR at JET. By taking the instrumental response function of TOFOR into account, we calculate time-of-flight NES weight functions that enable us to directly determine the velocity-space sensitivity of a given part of a measured time-of-flight spectrum from TOFOR.

  1. Invited Article: Characterization of background sources in space-based time-of-flight mass spectrometers

    SciTech Connect (OSTI)

    Gilbert, J. A.; Gershman, D. J.; Gloeckler, G.; Lundgren, R. A.; Zurbuchen, T. H.; Orlando, T. M.; McLain, J.; Steiger, R. von

    2014-09-15

    For instruments that use time-of-flight techniques to measure space plasma, there are common sources of background signals that evidence themselves in the data. The background from these sources may increase the complexity of data analysis and reduce the signal-to-noise response of the instrument, thereby diminishing the science value or usefulness of the data. This paper reviews several sources of background commonly found in time-of-flight mass spectrometers and illustrates their effect in actual data using examples from ACE-SWICS and MESSENGER-FIPS. Sources include penetrating particles and radiation, UV photons, energy straggling and angular scattering, electron stimulated desorption of ions, ion-induced electron emission, accidental coincidence events, and noise signatures from instrument electronics. Data signatures of these sources are shown, as well as mitigation strategies and design considerations for future instruments.

  2. Orion Flight Test Exploration Flight Test-1

    E-Print Network [OSTI]

    Rathbun, Julie A.

    Orion Flight Test Exploration Flight Test-1 PRESS KIT/December 2014 www.nasa.gov NP-2014-11-020-JSC National Aeronautics and Space Administration #12;#12;Orion Flight Test December 2014 Contents Section Page ........................................................................................... 28 i #12;Orion Flight Test ii December 2014 #12;Orion Flight Test December 2014 Flight Overview

  3. NASA Launches ATREX Space Network to Begin New Design Phase

    E-Print Network [OSTI]

    Christian, Eric

    Design Phase - 8 Dual Frequency Radar Arrives at Goddard - 9 Goddard Community Visitor Center Hosts TitanNASA Launches ATREX Pg 3 Space Network to Begin New Design Phase Pg 8 Visitor Center Hosts Titan://www.nasa.gov/centers/goddard/news/goddard-view.html Managing Editor: Trusilla Steele Editor: John M. Putman News items for publication in Goddard View must

  4. Proceedings of the Fifth NASA Goddard Space Flight Center Conference on Mass Storage Systems and Technologies, September 17-19, 1996 College Park, MD.

    E-Print Network [OSTI]

    of the resources required by individual applications and the aggregate demands made by a continually increasing to lead to better performance as perceived by users, the response time of distributed operations must response time significant enough to trigger customer dissatisfaction. In particular, we show how, after

  5. Workshop: Estudos de Ecossistemas usando Dados de Espectrmetros Imageadores (Ecosystem Studies using Imaging Spectrometer Coordenadora: Elizabeth M. Middleton (NASA/Goddard Space Flight Center)

    E-Print Network [OSTI]

    provide unique information to reduce uncertainties in global ecosystem models, including that from studiesWorkshop: Estudos de Ecossistemas usando Dados de Espectrômetros Imageadores (Ecosystem Studies

  6. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    Hubble Hardware ­ 4 World Space Party Draws Hundreds to Goddard ­ 6 "Goddard Career Firsts" Panel Efficiency Particulate Air (HEPA) filters in the World's largest Class 10,000 clean room at the Goddard Space), and the Solar Dynamics Observa- tory (SDO). As we approach Goddard's fiftieth anniversary, it is appropriate

  7. NASA Marshall Space Flight Center Improves Cooling System Performance: Best Management Practice Case Study #10: Cooling Towers (Fact Sheet)

    SciTech Connect (OSTI)

    Not Available

    2011-02-01

    National Aeronautics and Space Administration's (NASA) Marshall Space Flight Center (MSFC) has a longstanding sustainability program that revolves around energy and water efficiency as well as environmental protection. MSFC identified a problematic cooling loop with six separate compressor heat exchangers and a history of poor efficiency. The facility engineering team at MSFC partnered with Flozone Services, Incorporated to implement a comprehensive water treatment platform to improve the overall efficiency of the system.

  8. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 1 Issue 8 October 2005 Goddard Tenure - 4 Goddard Education GSRP Symposium - 5 2004-2005 NASA Leadership Development Program Graduates Honored - 6 Goddard Library Hosts Annual Open House Event - 7 Goddard Updates NASA Technology to Help

  9. Developing a risk management "flight simulator" for manned space programs : a user interface to a system dynamic simulation of system safety at NASA

    E-Print Network [OSTI]

    Friedenthal, Stephen R. (Stephen Roger)

    2006-01-01

    Simulators are a staple of any engineering project and manned space flight in particular. From pilot and crew training to maintenance and emergency repairs, very little is done without it first being thoroughly practiced ...

  10. Flight-Ready Robotic Servicing for Hubble Space Telescope: A White Paper

    E-Print Network [OSTI]

    Akin, David

    at the berthing fittings on the aft bulkhead, under supervisory ground control. Positioned by an extended version awaiting a flight opportunity. The Interim Control Module was developed by the Naval Research Laboratory. Should additional failures occur for which the servicing spacecraft carries spares, it can redock

  11. Flight hardware development for a space-based robotic assembly and servicing testbed

    E-Print Network [OSTI]

    McCarthy, Bryan Patrick

    2014-01-01

    Robotic assembly and servicing missions in space are becoming increasingly attractive for their potential to expand space capabilities and save money. Future missions may construct large systems on-orbit, service existing ...

  12. National Aeronautics and Space Administration MAVEN Orbit Insertion

    E-Print Network [OSTI]

    Mojzsis, Stephen J.

    National Aeronautics and Space Administration NASAfacts MAVEN Orbit Insertion Mars Atmosphere. MAVEN: Exploring Mars' climate history #12;National Aeronautics and Space Administration Goddard Space

  13. An integrated time-of-flight versus residual energy subsystem for a compact dual ion composition experiment for space plasmas

    SciTech Connect (OSTI)

    Desai, M. I.; McComas, D. J.; Allegrini, F.; Livi, S. A.; Ogasawara, K.; Ebert, R. W.; Weidner, S. E.; Alexander, N.

    2015-05-15

    We have developed a novel concept for a Compact Dual Ion Composition Experiment (CoDICE) that simultaneously provides high quality plasma and energetic ion composition measurements over 6 decades in ion energy in a wide variety of space plasma environments. CoDICE measures the two critical ion populations in space plasmas: (1) mass and ionic charge state composition and 3D velocity and angular distributions of ?10 eV/q–40 keV/q plasma ions—CoDICE-Lo and (2) mass composition, energy spectra, and angular distributions of ?30 keV–10 MeV energetic ions—CoDICE-Hi. CoDICE uses a common, integrated Time-of-Flight (TOF) versus residual energy (E) subsystem for measuring the two distinct ion populations. This paper describes the CoDICE design concept, and presents results of the laboratory tests of the TOF portion of the TOF vs. E subsystem, focusing specifically on (1) investigation of spill-over and contamination rates on the start and stop microchannel plate (MCP) anodes vs. secondary electron steering and focusing voltages, scanned around their corresponding model-optimized values, (2) TOF measurements and resolution and angular resolution, and (3) cross-contamination of the start and stop MCPs’ singles rates from CoDICE-Lo and -Hi, and (4) energy resolution of avalanche photodiodes near the lower end of the CoDICE-Lo energy range. We also discuss physical effects that could impact the performance of the TOF vs. E subsystem in a flight instrument. Finally, we discuss advantages of the CoDICE design concept by comparing with capabilities and resources of existing flight instruments.

  14. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 5, Issue 2 March 2009 GoddardViewGoddard Day at the Maryland Capitol-- Celebrating 50 Years of Space Exploration Pg 6 NASA Debuts Unique Movie Goddard Updates Agency Calendar Initiative ­ 2 Sunday Experiment Draws More Than 1,000 Visitors ­ 3 NASA

  15. NASA's Marshall Space Flight Center Saves Water With High-Efficiency Toilet and Urinal Program: Best Management Practice Case Study #6 - Toilets and Urinals (Fact Sheet)

    SciTech Connect (OSTI)

    Not Available

    2011-02-01

    The National Aeronautics and Space Administration's (NASA) Marshall Space Flight Center (MSFC) has a longstanding, successful sustainability program that focuses on energy and water efficiency as well as environmental protection. Because MSFC was built in the 1960s, most of the buildings house outdated, inefficient restroom fixtures. The facility engineering team at MSFC developed an innovative efficiency model for replacing these older toilets and urinals.

  16. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 3 Issue 10 August 2007 Space for Education and Discovery Pg 3 Goddard Space Scientists Earn Prestigious NASA Honors Pg 11 Space Shuttle and Discovery Pg 3 Goddard Space Scientists Earn Prestigious NASA Honors Pg 9 National Aeronautics and Space

  17. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    Hubble Hardware ­ 4 World Space Party Draws Hundreds to Goddard ­ 6 "Goddard Career Firsts" Panel for Strategy and Development. For the past several months, she has served as the chief architect in developing), and the Solar Dynamics Observa- tory (SDO). As we approach Goddard's fiftieth anniversary, it is appropriate

  18. GoddardView National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Christian, Eric

    and Proposal Integrated Review and Evaluation System (NSPIRES) - 7 Texas Instruments Uses NASA Facility to Test of the Mayo Clinic Health Risk Assessment (HRA) to identify your health risks, and to link to resourcesHealth Web portal and the Mayo Clinic Health Risk Assessment, go to http://www.ohp.nasa.gov and click

  19. GoddardView National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Christian, Eric

    refugee. It also made him a replica of Refugee, the tiny teddy bear that a Holocaust survivor, Sophie

  20. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 11 Issue 2 March 2015 #12;GoddardView Trending ­ 2 ENGAGE Sessions: Providing a Better Understanding of Goddard's Work ­ 3 Up, Up and Away! NASA and Exploration ­ 6 Nimoy and NASA: A Legacy Traversing Time and Space ­ 8 Students Find MMS as Source

  1. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 1 Issue 11 December 2005 Goddard, 5 NASA Satellites Track Record Breaking Hurricane Season - 6 Goddard Responds to Call for Aid - 7 Huygens Probe Descends to Titan - 7 Hubble Prospects the Moon for Resources - 8 NASA's Top Space

  2. Science Background for the Reprocessing and Goddard Satellite-based Surface Turbulent Fluxes

    E-Print Network [OSTI]

    1 Science Background for the Reprocessing and Goddard Satellite-based Surface Turbulent Fluxes, MD 20771 USA #12;2 Science Background for the Reprocessing and Goddard Satellite-based Surface

  3. Bipartite Ramsey Numbers and Zarankiewicz Wayne Goddard 1

    E-Print Network [OSTI]

    Goddard, Wayne

    Bipartite Ramsey Numbers and Zarankiewicz Numbers Wayne Goddard 1 School of Geological and Computer Ramsey number b(m, n) is the least positive integer b such that if the edges of K(b, b) are coloured are used to bound b(m, n) for m, n 6. Key words: Graphs, bipartite Ramsey numbers, Zarankiewicz, bicliques

  4. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 2 Issue 15 August 2006 Goddard Prize Pg 7 National Aeronautics and Space Administration www.nasa.gov Volume 2 Issue 15 August 2006 #12

  5. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 2 Issue 17 September 2006 GoddardView National Aeronautics and Space Administration www.nasa.gov Volume 2 Issue 17 September 2006 Earth

  6. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 3 Issue 6 April 2007 GoddardView National Aeronautics and Space Administration www.nasa.gov Volume 3 Issue 6 April 2007 Deep Impact Extended

  7. Goddard Hot Springs Geothermal Area | Open Energy Information

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QAsource History View New PagesSustainableGlynn County, Georgia: Energy Resources Jump to: navigation,Goddard Hot

  8. Goddard Pool & Spa Low Temperature Geothermal Facility | Open Energy

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QAsource History View New PagesSustainableGlynn County, Georgia: Energy Resources Jump to: navigation,Goddard

  9. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 2 Issue 18 October 2006 GoddardViewNASA at: http://www.nasa.gov/centers/goddard/news/index.html Managing Editor: Trusilla Steele Editor via e-mail at alittle@pop100.gsfc.nasa.gov. Ideas for new stories are welcome but will be published

  10. The Mid-Infrared Instrument for the James Webb Space Telescope, III: MIRIM, The MIRI Imager

    E-Print Network [OSTI]

    Bouchet, P; Lagage, P -O; Amiaux, J; Augueres, J -L; Bauwens, E; Blommaert, J A D L; Chen, C H; Detre, O H; Dicken, D; Dubreuil, D; Galdemard, Ph; Gastaud, R; Glasse, A; Gordon, K D; Gougnaud, F; Guillard, P; Justtanont, K; Krause, O; Leboeuf, D; Longval, Y; Martin, L; Mazy, E; Moreau, V; Olofsson, G; Ray, T P; Reess, J -M; Renotte, E; Ressler, M E; Ronayette, S; Salasca, S; Scheithauer, S; Sykes, J; Thelen, M P; Wells, M; Wright, D; Wright, G S

    2015-01-01

    In this article, we describe the MIRI Imager module (MIRIM), which provides broad-band imaging in the 5 - 27 microns wavelength range for the James Webb Space Telescope. The imager has a 0"11 pixel scale and a total unobstructed view of 74"x113". The remainder of its nominal 113"x113" field is occupied by the coronagraphs and the low resolution spectrometer. We present the instrument optical and mechanical design. We show that the test data, as measured during the test campaigns undertaken at CEA-Saclay, at the Rutherford Appleton Laboratory, and at the NASA Goddard Space Flight Center, indicate that the instrument complies with its design requirements and goals. We also discuss the operational requirements (multiple dithers and exposures) needed for optimal scientific utilization of the MIRIM.

  11. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 4, Issue 14 August 2008 Goddard of Aeronautics and Astronautics. Look for more details and information on LaunchFest at: http

  12. NASA's new modeling framework for integrating cloud processes explicitly within each grid column of a general circulation model can improve realism over the conventional model that

    E-Print Network [OSTI]

    Collett Jr., Jeffrey L.

    NASA's new modeling framework for integrating cloud processes explicitly within each grid column, AND SIMPSON--Laboratory for Atmospheres, NASA Goddard Space Flight Center, Greenbelt, Maryland; CHERN--Laboratory for Atmospheres, NASA Goddard Space Flight Center, Greenbelt, and Goddard Earth Sciences and Technology Center

  13. X-RAY SPECTRAL COMPONENTS OBSERVED IN THE AFTERGLOW OF GRB 130925A...

    Office of Scientific and Technical Information (OSTI)

    Center for Astronomy and Astrophysics, Post Bag 4, Ganeshkhind, Pune 411007 (India) NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States) DTU Space-National...

  14. TITLE AUTHORS SUBJECT SUBJECT RELATED DESCRIPTION PUBLISHER AVAILABILI...

    Office of Scientific and Technical Information (OSTI)

    Center for Astronomy and Astrophysics Post Bag Ganeshkhind Pune India Cenko S Bradley NASA Goddard Space Flight Center Greenbelt MD United States Christensen Finn E DTU Space...

  15. TITLE AUTHORS SUBJECT SUBJECT RELATED DESCRIPTION PUBLISHER AVAILABILI...

    Office of Scientific and Technical Information (OSTI)

    Astrophysics Laboratory Columbia University New York NY United States Zhang William W NASA Goddard Space Flight Center Greenbelt MD United States Boggs Steven E Space Sciences...

  16. Marshall Space Flight Center (MSFC) Agency Introduction: The FY 2012 budget request for NASA is $18.7 billion, the FY 2010 enacted

    E-Print Network [OSTI]

    research and test expertise, scientists and engineers also work in partnership with academic institutions centers with over 4.5 million square feet of space including test, manufacturing and research facilities on the Ares I launch vehicle, into the development of a new heavy-lift rocket, the Space Launch System

  17. Studying Altocumulus Plus Virga with Ground-based Active and Passive Remote Sensors Zhien Wang1, Kenneth Sassen2, David Whiteman3, and Belay Demoz3 1University of Maryland, Baltimore County, Catonsville, MD 21228 2University of Alaska, Fairbanks, Alaska 99775 3NASA Goddard Space Flight Center, Greenbelt, MD 20771 E-mail: zhien@agnes.gsfc.nasa.gov

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantityBonneville Power AdministrationRobust,Field-effect PhotovoltaicsStructure andChallenge | Department,Aerosol

  18. Studying Altocumulus Plus Virga with Ground-based Active and Passive Remote Sensors Zhien Wang1, Kenneth Sassen2, David Whiteman3, and Belay Demoz3 1University of Maryland, Baltimore County, Catonsville, MD 21228 2University of Alaska, Fairbanks, Alaska 99775 3NASA Goddard Space Flight Center, Greenbelt, MD 20771 E-mail: zhien@agnes.gsfc.nasa.gov

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantityBonneville Power AdministrationRobust,Field-effect PhotovoltaicsStructure andChallenge | Department,AerosolSeasonal and

  19. Space

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home RoomPreservation ofAlbuquerque|SensitiveApril 2, 2014 Smith Named as NewAprilSpace

  20. Resubmitted to ApJ March 4 2005 On the Afterglow and Host Galaxy of GRB 021004: A

    E-Print Network [OSTI]

    Fynbo, Johan

    , USA 12 NASA/Marshall Space Flight Center, National Space Science and Technology Center (NSSTC), SD­50 Nieuwland Science Hall, Notre Dame IN 46556, USA 15 Swift Science Center, Goddard Space Flight Center, Code

  1. Venus Transit at Goddard Visitor Center Oh, the Places We'll Go

    E-Print Network [OSTI]

    Christian, Eric

    reader Ray Rubilotta, Acting Director of the Management Operations Directorate, said, "It re-charged my own `personal battery' for the day to be around the children. The energy, interest, enthusiasm to the Goddard Visitor Center tries to see Venus as it crosses in front of the Sun. Photo Credit: NASA

  2. CpSc212 Goddard Notes Chapter 5 More about Classes

    E-Print Network [OSTI]

    Goddard, Wayne

    . The header file lists the data and gives prototypes for the functions. Many people put the 10 #12;public Mathematical functions are available in the library cmath. Note that angles are repre- sented in radiansCpSc212 ­ Goddard ­ Notes Chapter 5 More about Classes 5.1 More about Member Functions One can

  3. Goddard technologists are working on laser instrumentation that will characterize the Martian atmosphere and improve

    E-Print Network [OSTI]

    Christian, Eric

    , detectors, and other components needed to build a completesystem. Laser/Lidar Technologies for Exploration atmosphere and improve landing safety on Mars and other solar system bodies. First Nano Device to Fly Systems Research and Technology Funds Two Goddard researchers have received funding from

  4. The A.J. Goddard: Reconstruction and Material Culture of a Klondike Gold Rush Sternwheeler 

    E-Print Network [OSTI]

    Thomas, Lindsey Hall

    2012-10-19

    The A.J. Goddard, a steamboat built for the Klondike Gold Rush of 1897-1898, wrecked in 1901 on Lake Laberge, Yukon Territory, where it lay undisturbed until its rediscovery in 2008 by the Yukon River Survey Project, directed by John Pollack...

  5. Project Management in NASA Mars Climate Orbiter

    E-Print Network [OSTI]

    Rhoads, James

    by the Mars Climate Orbiter Mishap Investigation Board F. Recurring Themes From Failure Investigations and Control Center Navigation and Control Center Goddard Space Flight Center Goddard Space Flight Center Merwarth NASA/GSFC-retired Expert in ground operations & flight software development Moshe F. Rubinstein

  6. Fall, recovery, and characterization of the Novato L6 chondrite breccia Peter JENNISKENS1,2*

    E-Print Network [OSTI]

    Zare, Richard N.

    , California 94550, USA 14 Institute of Meteoritics, University of New Mexico, Albuquerque, New Mexico 87131 Freising, Germany 27 Solar System Exploration Division, NASA Goddard Space Flight Center, Greenbelt

  7. NGC 404: A REJUVENATED LENTICULAR GALAXY ON A MERGER-INDUCED...

    Office of Scientific and Technical Information (OSTI)

    NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States) Publication Date: 2010-05-01 OSTI Identifier: 21448922 Resource Type: Journal Article Resource Relation:...

  8. "Title","Creator/Author","Publication Date","OSTI Identifier...

    Office of Scientific and Technical Information (OSTI)

    and Astrophysics, Post Bag 4, Ganeshkhind, Pune 411007 (India); Cenko, S. Bradley NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States); Christensen, Finn E....

  9. X-RAY SPECTRAL COMPONENTS OBSERVED IN THE AFTERGLOW OF GRB 130925A...

    Office of Scientific and Technical Information (OSTI)

    and Astrophysics, Post Bag 4, Ganeshkhind, Pune 411007 (India); Cenko, S. Bradley NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States); Christensen, Finn E....

  10. NuSTAR and Suzaku Tomsick, John A.; Boggs, Steven E.; Craig,...

    Office of Scientific and Technical Information (OSTI)

    via del Fosso del Cavaliere, I-00133 Roma (Italy); Pottschmidt, Katja CRESST and NASA Goddard Space Flight Center, Astrophysics Science Division, Code 661, Greenbelt, MD...

  11. THE NUCLEAR SPECTROSCOPIC TELESCOPE ARRAY (NuSTAR) HIGH-ENERGY...

    Office of Scientific and Technical Information (OSTI)

    Columbia University, New York, NY 10027 (United States); Zhang, William W. NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States); Boggs, Steven E....

  12. STUDYING LARGE- AND SMALL-SCALE ENVIRONMENTS OF ULTRAVIOLET LUMINOUS

    Office of Scientific and Technical Information (OSTI)

    CA 91101 (United States); Neff, Susan G. Laboratory for Astronomy and Solar Physics, NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States), E-mail:...

  13. "Title","Creator/Author","Publication Date","OSTI Identifier...

    Office of Scientific and Technical Information (OSTI)

    Columbia University, New York, NY 10027 (United States); Zhang, William W. NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States); Boggs, Steven E....

  14. "Title","Creator/Author","Publication Date","OSTI Identifier...

    Office of Scientific and Technical Information (OSTI)

    CA 91101 (United States); Neff, Susan G. Laboratory for Astronomy and Solar Physics, NASA Goddard Space Flight Center, Greenbelt, MD 20771 (United States), E-mail:...

  15. TITLE AUTHORS SUBJECT SUBJECT RELATED DESCRIPTION PUBLISHER AVAILABILI...

    Office of Scientific and Technical Information (OSTI)

    INAF IAPS via del Fosso del Cavaliere I Roma Italy Pottschmidt Katja CRESST and NASA Goddard Space Flight Center Astrophysics Science Division Code Greenbelt MD United...

  16. "Title","Creator/Author","Publication Date","OSTI Identifier...

    Office of Scientific and Technical Information (OSTI)

    via del Fosso del Cavaliere, I-00133 Roma (Italy); Pottschmidt, Katja CRESST and NASA Goddard Space Flight Center, Astrophysics Science Division, Code 661, Greenbelt, MD...

  17. Distant origins of Arctic black carbon: A Goddard Institute for Space Studies ModelE experiment

    E-Print Network [OSTI]

    %) and from biomass (28%) (with slightly more than half of biomass coming from north of 40°N); North America ``soot,'' is derived from the incomplete combustion of fossil fuels (primarily coal and diesel) and from

  18. The REgolith X-ray Imaging Spectrometer flight model : structural design, analysis, and testing

    E-Print Network [OSTI]

    Carte, David Brad

    2015-01-01

    Engineers of space flight programs face unique technical challenges created by the space environment in which these systems operate. High costs and increasing complexity of space programs create a greater demand for mission ...

  19. Dynamic and thermal control of an electromagnetic formation flight testbed

    E-Print Network [OSTI]

    Neave, Matthew D. (Matthew David)

    2005-01-01

    Formation flight of multiple spacecraft is an emerging method for completing complex space missions in an efficient manner. A limitation found in maintaining such formations is the need for precise control at all times. ...

  20. Space Shuttle Program Status

    E-Print Network [OSTI]

    Waliser, Duane E.

    Payload: 36th ISS flight (ULF6), EXPRESS Logistics Carrier 3 (ELC3), Alpha Magnetic Spectrometer (AMS;8 Transition #12;9 Major Space Shuttle Program Facilities Reusable Solid Rocket Motor ATK Thiokol Propulsion

  1. Analytical and experimental studies of leak location and environment characterization for the international space station

    SciTech Connect (OSTI)

    Woronowicz, Michael; Blackmon, Rebecca; Brown, Martin; Abel, Joshua; Hawk, Doug; Autrey, David; Glenn, Jodie; Bond, Tim; Buffington, Jesse; Cheng, Edward; Ma, Jonathan; Rossetti, Dino; DeLatte, Danielle; Garcia, Kelvin; Mohammed, Jelila; Montt de Garcia, Kristina; Perry, Radford; Tull, Kimathi; Warren, Eric

    2014-12-09

    The International Space Station program is developing a robotically-operated leak locator tool to be used externally. The tool would consist of a Residual Gas Analyzer for partial pressure measurements and a full range pressure gauge for total pressure measurements. The primary application is to demonstrate the ability to detect NH{sub 3} coolant leaks in the ISS thermal control system. An analytical model of leak plume physics is presented that can account for effusive flow as well as plumes produced by sonic orifices and thruster operations. This model is used along with knowledge of typical RGA and full range gauge performance to analyze the expected instrument sensitivity to ISS leaks of various sizes and relative locations (“directionality”). The paper also presents experimental results of leak simulation testing in a large thermal vacuum chamber at NASA Goddard Space Flight Center. This test characterized instrument sensitivity as a function of leak rates ranging from 1 lb{sub m/}/yr. to about 1 lb{sub m}/day. This data may represent the first measurements collected by an RGA or ion gauge system monitoring off-axis point sources as a function of location and orientation. Test results are compared to the analytical model and used to propose strategies for on-orbit leak location and environment characterization using the proposed instrument while taking into account local ISS conditions and the effects of ram/wake flows and structural shadowing within low Earth orbit.

  2. National Aeronautics and Space Administration organizations around the nation, and is led

    E-Print Network [OSTI]

    Rathbun, Julie A.

    National Aeronautics and Space Administration NASAfacts organizations around the nation, and is led;National Aeronautics and Space Administration George C. Marshall Space Flight Center Huntsville, AL 35812

  3. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 3 Issue 12 September 2007 SDO of Goddard employees, contractors, and retirees. A PDF version is available online at: http://www.nasa may submit contribu- tions to the editor via e-mail at alana.m.little@nasa.gov. Ideas for new stories

  4. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 2 Issue 10 June 2006 GoddardViewFirst Images from NASA's Cloudsat Pg 2 Unintentional Intolerance Pg 3 Astronomy Hits the Theater from NASA's Cloudsat - 2 Unintentional Tolerance- 3 Inexpensive Detector Sees the Invisible, In Color

  5. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 11 Issue 1 February 2015 #12;GoddardView Trending ­ 2 NASA's New Radiometer Tunes in to Soil's Frequency ­ 3 Innovation in Content" Captivates Visitor Center Guests ­ 8 NASA Team Develops New Communications System to Break Through Noise ­ 9

  6. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 4, Issue 11 June 2008 GoddardViewNASA Composite Carrier for Hubble Servicing Mission Pg 4 NASA Technology Contributes to National Security Pg 6 One Million People Going to the Moon ­ 2 NASA Exhibit Pays Tribute to Fallen Heroes of Spaceflight

  7. Boone Schirmer and the Early Days of the Philippines Information Bulletin, Friends of the Filipino People, and the Philippines Program at Goddard-Cambridge

    E-Print Network [OSTI]

    Gaerlan, Barbara S.

    2006-01-01

    and the Early Days of the Philippines Information Bulletin,the Filipino People, and the Philippines Program at Goddard-publication of the journal Philippines Information Bulletin.

  8. National Aeronautical and Space Administration (NASA) Johnson Space Flight

    Broader source: Energy.gov (indexed) [DOE]

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of Natural GasAdjustmentsShirleyEnergyTher i nAand DOEDepartment ofProgram | DepartmentEnergy6 3 9 12 6 3 9 12 6 3 9

  9. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

    E-Print Network [OSTI]

    Rathbun, Julie A.

    NATIONAL AERONAUTICS AND SPACE ADMINISTRATION OFFICE OF MANNED SPACE FLIGHT DEPARTMENT OF THE ARMY of the Chief of Engineers Washington, D. C. and National Aeronautics and Space Administration Office of Manned of the National Aeronautics and Space Administration concept development program for LESA and was conducted under

  10. http://umbra.nascom.nasa.gov/soho/ SOHO_final_report.html

    E-Print Network [OSTI]

    Rhoads, James

    _______________________________ John Credland Head, Science Projects Department ESA/ESTEC _______________________________ Dr. H's Goddard Space Flight Center _______________________________ Alan Smith Head, Flight Operations Division checkout and the transition from low earth orbit into a halo orbit around the Lagrangian L1 point

  11. ZEST flight test experiments, Kauai Test Facility, Hawaii. Test report

    SciTech Connect (OSTI)

    Cenkci, M.J.

    1991-07-01

    The Strategic Defense Initiative Organization (SDIO) is proposing to execute two ZEST flight experiments to obtain information related to the following objectives: validation of payload modeling; characterization of a high energy release cloud; and documentation of scientific phenomena that may occur as a result of releasing a high energy cloud. The proposed action is to design, develop, launch, and detonate two payloads carrying high energy explosives. Activities required to support this proposal include: (1) execution of component assembly tests at Space Data Division (SDD) in Chandler, Arizona and Los Alamos National Laboratory (LANL) in Los Alamos, New Mexico, and (2) execution of pre-flight flight test activities at Kauai Test Facility.

  12. Densitometric analysis of IIaO film flown aboard the space shuttle transportation system STS-3, STS-8, and STS-7. Semiannual report, December 1986

    SciTech Connect (OSTI)

    Hammond, E.C. Jr.; Peters, K.A.; Atkinson, P.F.

    1986-01-01

    Three canisters of IIaO film were prepared along with packets of color film from the National Geographic Society, which were then placed on the Space Shuttle number3. The ultimate goal was to obtain reasonably accurate data concerning the background fogging effects on IIaO film as it relates to the film's total environmental experience. This includes: the ground based packing, and loading of the film from Goddard Space Flight Center to Cape Kennedy; the effects of the solar wind, humidity, and cosmic rays; the Van Allen Belt radiation exposure; various thermal effect; reentry and off-loading of the film during take off, and 8 day, 3 hour 15 minutes orbits. The total densitometric change caused by all of the above factors were examined. The results of these studies have implications for the utilization of IIaO spectroscopic film on the future shuttle and space lab missions. These responses to standard photonic energy sources will have immediate application for the uneven responses of the film photographing a star field in a terrestrial or extraterrestrial environment with associated digital imaging equipment.

  13. Ban on US–China space-program ties means missed opportunities for NASA

    SciTech Connect (OSTI)

    Kramer, David

    2013-12-15

    Sino-US cooperation could stretch budgets and benefit both countries in space science and human flight.

  14. Flight Path 12

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast This flight path is

  15. Flight Path 12

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast This flight path

  16. Flight Path 12

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast This flight

  17. Flight Path 5 - About

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast(ER1) Target 1 Flight

  18. Flight Path 5

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfateSciTechtail.Theory ofDid you not find whatGasEnergyfeature photoTheory05 Target 1 Flight Path 05

  19. Flight Path Target 2

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfateSciTechtail.Theory ofDid you not find whatGasEnergyfeature photoTheory05 Target 1 Flight Path90L2

  20. Flight Paths at WNR

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfateSciTechtail.Theory ofDid you not find whatGasEnergyfeature photoTheory05 Target 1 FlightNeutron

  1. PHARAO Laser Source Flight Model: Design and Performances

    E-Print Network [OSTI]

    Lévčque, Thomas; Esnault, François-Xavier; Delaroche, Christophe; Massonnet, Didier; Grosjean, Olivier; Buffe, Fabrice; Torresi, Patrizia; Bomer, Thierry; Pichon, Alexandre; Béraud, Pascal; Lelay, Jean-Pierre; Thomin, Stéphane; Laurent, Philippe

    2015-01-01

    In this paper, we describe the design and the main performances of the PHARAO laser source flight model. PHARAO is a laser cooled cesium clock specially designed for operation in space and the laser source is one of the main sub-systems. The flight model presented in this work is the first remote-controlled laser system designed for spaceborne cold atom manipulation. The main challenges arise from mechanical compatibility with space constraints, which impose a high level of compactness, a low electric power consumption, a wide range of operating temperature and a vacuum environment. We describe the main functions of the laser source and give an overview of the main technologies developed for this instrument. We present some results of the qualification process. The characteristics of the laser source flight model, and their impact on the clock performances, have been verified in operational conditions.

  2. Time-of-flight radio location system

    DOE Patents [OSTI]

    McEwan, Thomas E. (Livermore, CA)

    1996-01-01

    A bi-static radar configuration measures the direct time-of-flight of a transmitted RF pulse and is capable of measuring this time-of-flight with a jitter on the order of about one pico-second, or about 0.01 inch of free space distance for an electromagnetic pulse over a range of about one to ten feet. A transmitter transmits a sequence of electromagnetic pulses in response to a transmit timing signal, and a receiver samples the sequence of electromagnetic pulses with controlled timing in response to a receive timing signal, and generates a sample signal in response to the samples. A timing circuit supplies the transmit timing signal to the transmitter and supplies the receive timing signal to the receiver. The receive timing signal causes the receiver to sample the sequence of electromagnetic pulses such that the time between transmission of pulses in the sequence and sampling by the receiver sweeps over a range of delays. The receive timing signal sweeps over the range of delays in a sweep cycle such that pulses in the sequence are sampled at the pulse repetition rate, and with different delays in the range of delays to produce a sample signal representing magnitude of a received pulse in equivalent time. Automatic gain control circuitry in the receiver controls the magnitude of the equivalent time sample signal. A signal processor analyzes the sample signal to indicate the time-of-flight of the electromagnetic pulses in the sequence.

  3. Time-of-flight radio location system

    DOE Patents [OSTI]

    McEwan, T.E.

    1996-04-23

    A bi-static radar configuration measures the direct time-of-flight of a transmitted RF pulse and is capable of measuring this time-of-flight with a jitter on the order of about one pico-second, or about 0.01 inch of free space distance for an electromagnetic pulse over a range of about one to ten feet. A transmitter transmits a sequence of electromagnetic pulses in response to a transmit timing signal, and a receiver samples the sequence of electromagnetic pulses with controlled timing in response to a receive timing signal, and generates a sample signal in response to the samples. A timing circuit supplies the transmit timing signal to the transmitter and supplies the receive timing signal to the receiver. The receive timing signal causes the receiver to sample the sequence of electromagnetic pulses such that the time between transmission of pulses in the sequence and sampling by the receiver sweeps over a range of delays. The receive timing signal sweeps over the range of delays in a sweep cycle such that pulses in the sequence are sampled at the pulse repetition rate, and with different delays in the range of delays to produce a sample signal representing magnitude of a received pulse in equivalent time. Automatic gain control circuitry in the receiver controls the magnitude of the equivalent time sample signal. A signal processor analyzes the sample signal to indicate the time-of-flight of the electromagnetic pulses in the sequence. 7 figs.

  4. JACEE long duration balloon flights

    SciTech Connect (OSTI)

    Burnett, T.; Iwai, J.; Lord, J.J.; Strausz, S.; Wilkes, R.J. ); Dake, S.; Oda, H. ); Miyamura, O. ); Fuki, M. ); Jones, W.V. ); Gregory, J.; Hayashi, T.; Takahashi, U. ); Tominaga,

    1989-01-01

    JACEE balloon-borne emulsion chamber detectors are used to observe the spectra and interactions of cosmic ray protons and nuclei in the energy range 1-100A TeV. Experience with long duration mid-latitude balloon flights and characteristics of the detector system that make it ideal for planned Antarctic balloon flights are discussed. 5 refs., 2 figs.

  5. AERODYNAMICS AND DESIGN FOR ULTRA-LOW REYNOLDS NUMBER FLIGHT

    E-Print Network [OSTI]

    Stanford University

    AERODYNAMICS AND DESIGN FOR ULTRA-LOW REYNOLDS NUMBER FLIGHT A DISSERTATION SUBMITTED at Reynolds numbers below 10,000, here termed ultra-low Reynolds numbers. The effects of airfoil geometry at ultra-low Reynolds numbers. To further explore this design space, the flow solver has been coupled

  6. Global Optimization for the Design of Space Trajectories

    E-Print Network [OSTI]

    2008-11-21

    Lambert's problem and arc Given two points in space and the time of flight between ... points can be calculated by solving a Lambert's problem, which basically.

  7. Autonomous helicopter flight via Reinforcement Learning

    E-Print Network [OSTI]

    Sastry, S. Shankar

    Autonomous helicopter flight via Reinforcement Learning Andrew Y. Ng Stanford University Stanford 94720 Abstract Autonomous helicopter flight represents a challenging control problem, with complex to autonomous helicopter flight. We first fit a stochastic, nonlinear model of the helicopter dynamics. We

  8. Autonomous helicopter flight via reinforcement learning

    E-Print Network [OSTI]

    Jordan, Michael I.

    Autonomous helicopter flight via reinforcement learning Andrew Y. Ng Stanford University Stanford 94720 Abstract Autonomous helicopter flight represents a challenging control problem, with complex to autonomous helicopter flight. We first fit a stochastic, nonlinear model of the helicopter dynamics. We

  9. A flight of behavior analysis

    E-Print Network [OSTI]

    Baer, Donald M.

    1981-01-01

    Comments on J. Michael's (1980) discussion on the flight from behavior analysis by looking positively upon the following points: The applied people are largely new personnel who are not quick to apply new basic findings and who do not relate...

  10. Citizen Report National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Citizen Report National Aeronautics and Space Administration Dryden Flight Research Center A look/Carla Thomas #12;Citizen Report Fiscal Year 2012 Dryden Flight Research Center, located on the western edge the low-speed stability and control of a low-noise version of a proposed future Hybrid Wing Body aircraft

  11. Time-of-flight radio location system

    DOE Patents [OSTI]

    McEwan, T.E.

    1997-08-26

    A bi-static radar configuration measures the direct time-of-flight of a transmitted RF pulse and is capable of measuring this time-of-flight with a jitter on the order of about one pico-second, or about 0.01 inch of free space distance for an electromagnetic pulse over a range of about one to ten feet. A transmitter transmits a sequence of electromagnetic pulses in response to a transmit timing signal, and a receiver samples the sequence of electromagnetic pulses with controlled timing in response to a receive timing signal, and generates a sample signal in response to the samples. A timing circuit supplies the transmit timing signal to the transmitter and supplies the receive timing signal to the receiver. The receive timing signal causes the receiver to sample the sequence of electromagnetic pulses such that the time between transmission of pulses in the sequence and sampling by the receiver sweeps over a range of delays. The receive timing signal sweeps over the range of delays in a sweep cycle such that pulses in the sequence are sampled at the pulse repetition rate, and with different delays in the range of delays to produce a sample signal representing magnitude of a received pulse in equivalent time. Automatic gain control circuitry in the receiver controls the magnitude of the equivalent time sample signal. A signal processor analyzes the sample signal to indicate the time-of-flight of the electromagnetic pulses in the sequence. The sample signal in equivalent time is passed through an envelope detection circuit, formed of an absolute value circuit followed by a low pass filter, to convert the sample signal to a unipolar signal to eliminate effects of antenna misorientation. 8 figs.

  12. Time-of-flight radio location system

    DOE Patents [OSTI]

    McEwan, Thomas E. (Livermore, CA)

    1997-01-01

    A bi-static radar configuration measures the direct time-of-flight of a transmitted RF pulse and is capable of measuring this time-of-flight with a jitter on the order of about one pico-second, or about 0.01 inch of free space distance for an electromagnetic pulse over a range of about one to ten feet. A transmitter transmits a sequence of electromagnetic pulses in response to a transmit timing signal, and a receiver samples the sequence of electromagnetic pulses with controlled timing in response to a receive timing signal, and generates a sample signal in response to the samples. A timing circuit supplies the transmit timing signal to the transmitter and supplies the receive timing signal to the receiver. The receive timing signal causes the receiver to sample the sequence of electromagnetic pulses such that the time between transmission of pulses in the sequence and sampling by the receiver sweeps over a range of delays. The receive timing signal sweeps over the range of delays in a sweep cycle such that pulses in the sequence are sampled at the pulse repetition rate, and with different delays in the range of delays to produce a sample signal representing magnitude of a received pulse in equivalent time. Automatic gain control circuitry in the receiver controls the magnitude of the equivalent time sample signal. A signal processor analyzes the sample signal to indicate the time-of-flight of the electromagnetic pulses in the sequence. The sample signal in equivalent time is passed through an envelope detection circuit, formed of an absolute value circuit followed by a low pass filter, to convert the sample signal to a unipolar signal to eliminate effects of antenna misorientation.

  13. Free-flight experiments in LISA Pathfinder

    E-Print Network [OSTI]

    M. Armano; H. Audley; G. Auger; J. Baird; P. Binetruy; M. Born; D. Bortoluzzi; N. Brandt; A. Bursi; M. Caleno; A. Cavalleri; A. Cesarini; M. Cruise; C. Cutler; K. Danzmann; I. Diepholz; R. Dolesi; N. Dunbar; L. Ferraioli; V. Ferroni; E. Fitzsimons; M. Freschi; J. Gallegos; C. Garcia. Marirrodriga; R. Gerndt; LI. Gesa; F. Gibert; D. Giardini; R. Giusteri; C. Grimani; I. Harrison; G. Heinzel; M. Hewitson; D. Hollington; M. Hueller; J. Huesler; H. Inchauspe; O. Jennrich; P. Jetzer; B. Johlander; N. Karnesis; B. Kaune; N. Korsakova; C. Killow; I. Lloro; R. Maarschalkerweerd; S. Madden; P. Maghami; D. Mance; V. Martin; F. Martin-Porqueras; I. Mateos; P. McNamara; J. Mendes; L. Mendes; A. Moroni; M. Nofrarias; S. Paczkowski; M. Perreur-Lloyd; A. Petiteau; P. Pivato; E. Plagnol; P. Prat; U. Ragnit; J. Ramos-Castro; J. Reiche; J. A. Romera. Perez; D. Robertson; H. Rozemeijer; G. Russano; P. Sarra; A. Schleicher; J. Slutsky; C. F. Sopuerta; T. Sumner; D. Texier; J. Thorpe; C. Trenkel; H. B. Tu; D. Vetrugno; S. Vitale; G. Wanner; H. Ward; S. Waschke; P. Wass; D. Wealthy; S. Wen; W. Weber; A. Wittchen; C. Zanoni; T. Ziegler; P. Zweifel

    2014-12-29

    The LISA Pathfinder mission will demonstrate the technology of drag-free test masses for use as inertial references in future space-based gravitational wave detectors. To accomplish this, the Pathfinder spacecraft will perform drag-free flight about a test mass while measuring the acceleration of this primary test mass relative to a second reference test mass. Because the reference test mass is contained within the same spacecraft, it is necessary to apply forces on it to maintain its position and attitude relative to the spacecraft. These forces are a potential source of acceleration noise in the LISA Pathfinder system that are not present in the full LISA configuration. While LISA Pathfinder has been designed to meet it's primary mission requirements in the presence of this noise, recent estimates suggest that the on-orbit performance may be limited by this `suspension noise'. The drift-mode or free-flight experiments provide an opportunity to mitigate this noise source and further characterize the underlying disturbances that are of interest to the designers of LISA-like instruments. This article provides a high-level overview of these experiments and the methods under development to analyze the resulting data.

  14. On the effect of dust particles on global CCN and cloud droplet number1 V.A. Karydis1

    E-Print Network [OSTI]

    Nenes, Athanasios

    Institute of Technology, Atlanta,4 GA5 3 SABIC-Innovative Plastics, Selkirk, NY6 4 NASA Goddard Space Flight, Georgia Institute of Technology, Atlanta, GA3 2 School of Chemical and Biomolecular Engineering, Georgia

  15. The Astrophysical Journal, 664:L91L94, 2007 August 1 2007. The American Astronomical Society. All rights reserved. Printed in U.S.A.

    E-Print Network [OSTI]

    California at Santa Cruz, University of

    wind nebulae (PWNe; Aharonian et al. 2005c), and molecular clouds (Aharonian et al. 2006a) as emitters Autonoma de Mexico, DF, Mexico. 9 NASA Goddard Space Flight Center, Greenbelt, MD. 10 University of New

  16. Four-winged flapping flyer in forward flight

    E-Print Network [OSTI]

    Godoy-Diana, Ramiro; Centeno, Mariana; Weinreb, Alexis; Thiria, Benjamin

    2015-01-01

    We study experimentally a four-winged flapping flyer with chord-wise flexible wings in a self-propelled setup. For a given physical configuration of the flyer (i.e. fixed distance between the forewing and hindwing pairs and fixed wing flexibility), we explore the kinematic parameter space constituted by the flapping frequency and the forewing-hindwing phase lag. Cruising speed and consumed electric power measurements are performed for each point in the $(f,\\varphi)$ parameter space and allow us to discuss the problem of performance and efficiency in four-winged flapping flight. We show that different phase-lags are needed for the system to be optimised for fastest flight or lowest energy consumption. A conjecture of the underlying mechanism is proposed in terms of the coupled dynamics of the forewing-hindwing phase lag and the deformation kinematics of the flexible wings.

  17. Time-of-flight direct recoil ion scattering spectrometer

    DOE Patents [OSTI]

    Krauss, A.R.; Gruen, D.M.; Lamich, G.J.

    1994-09-13

    A time-of-flight direct recoil and ion scattering spectrometer beam line is disclosed. The beam line includes an ion source which injects ions into pulse deflection regions and separated by a drift space. A final optics stage includes an ion lens and deflection plate assembly. The ion pulse length and pulse interval are determined by computerized adjustment of the timing between the voltage pulses applied to the pulsed deflection regions. 23 figs.

  18. Time of flight mass spectrometer

    DOE Patents [OSTI]

    Ulbricht, Jr., William H. (Arvada, CO)

    1984-01-01

    A time-of-flight mass spectrometer is described in which ions are desorbed from a sample by nuclear fission fragments, such that desorption occurs at the surface of the sample impinged upon by the fission fragments. This configuration allows for the sample to be of any thickness, and eliminates the need for complicated sample preparation.

  19. Laminar Flow Control Flight Experiment Design 

    E-Print Network [OSTI]

    Tucker, Aaron 1975-

    2012-11-29

    Demonstration of spanwise-periodic discrete roughness element laminar flow control (DRE LFC) technology at operationally relevant flight regimes requires extremely stable flow conditions in flight. A balance must be struck ...

  20. AE 419: Aircraft Flight Mechanics Spring 2015

    E-Print Network [OSTI]

    Lee, Tonghun

    AE 419: Aircraft Flight Mechanics Spring 2015 Course Information (Tentative) Instructor: Prof. M. S, cruise, level turn, and energy methods; longitudinal, directional, and lateral static stability graduate hours Textbook: Thomas Yechout, et al. Introduction to Aircraft Flight Mechanics: Performance

  1. 4 YEAR FLIGHT PLAN: BFA in Painting

    E-Print Network [OSTI]

    Fernandez, Eduardo

    4 YEAR FLIGHT PLAN: BFA in Painting FAU is committed to your success as a student. One way we Name: Z: Program: Date: Advisor: Contact: Flight Plan: BFA in Painting NOTE: Some students may

  2. Electromagnetic Formation Flight of Satellite Arrays

    E-Print Network [OSTI]

    Electromagnetic Formation Flight of Satellite Arrays Daniel W. Kwon and David W. Miller February 2005 SSL # 2-05 #12;#12;Electromagnetic Formation Flight of Satellite Arrays By DANIEL W. KWON S;#12;Electromagnetic Formation Flight of Satellite Arrays by DANIEL W. KWON Submitted to the Department of Aeronautics

  3. NASA Marshall Space Flight Center Improves Cooling System Performance |

    Broader source: Energy.gov (indexed) [DOE]

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of Natural GasAdjustmentsShirleyEnergyTher i nAand DOEDepartment of Energy Motion toCITIZENSHarris, withNASADepartment

  4. - FLIGHT -

    Broader source: Energy.gov (indexed) [DOE]

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of Natural GasAdjustmentsShirleyEnergyTher i n c i p a l De p u t y A s s i s t a n t S e c r eEnergyHVACSecondAVIATION

  5. Flight Path 14 - About DANCE

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast This flight(DANCE)

  6. Flight Path 14 - About DANCE

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast This flight(DANCE)

  7. Flight Path 14 - About DANCE

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast This flight(DANCE)

  8. Flight Path 60R - GEANIE

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfateSciTechtail.Theory ofDid you not find whatGasEnergyfeature photoTheory05 Target 1 Flight Path

  9. Flight Path 90L - TPC

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfateSciTechtail.Theory ofDid you not find whatGasEnergyfeature photoTheory05 Target 1 Flight Path90L

  10. Airbus Toulouse Flight test data centre. Diagnosis and treatment of noisy vibration flight test data.

    E-Print Network [OSTI]

    Dobigeon, Nicolas

    Airbus Toulouse ­ Flight test data centre. Diagnosis and treatment of noisy vibration flight test data. The trainee will work within flight test vibration analysis team.The main missions and activities are the followings: - Use an automatic tool of vibration data quality defaults detection; evaluate this tool

  11. Flight Software Group The LASP Flight Software Group has a rich history of

    E-Print Network [OSTI]

    Mojzsis, Stephen J.

    development life-cycle. Software quality assurance engineers ensure compliance and perform audits. LASP usesFlight Software Group The LASP Flight Software Group has a rich history of developing flight software for planetary and earth-orbiting missions, beginning as early as the Galileo mission

  12. 4 YEAR FLIGHT PLAN: BFA in Ceramics

    E-Print Network [OSTI]

    Fernandez, Eduardo

    4 YEAR FLIGHT PLAN: BFA in Ceramics FAU is committed to your success as a student. One way we Name: Z: Program: Date: Advisor: Contact: Flight Plan: BFA in Ceramics NOTE: Some students may from the college Student Advising Services (SAS). Students that are admitted to the BFA in Ceramics

  13. Free flight of the mosquito Aedes aegypti

    E-Print Network [OSTI]

    Iams, S M

    2012-01-01

    High speed video observations of free flying male Aedes aegypti mosquitoes, the dengue and yellow fever vector, along with custom measurement methods, enable measurement of wingbeat frequency, body position and body orientation of mosquitoes during flight. We find these mosquitoes flap their wings at approximately 850 Hz. We also generate body yaw, body pitch and wing deviation measurements with standard deviations of less than 1 degree and find that sideways velocity and acceleration are important components of mosquito motion. Rapid turns involving changes in flight direction often involve large sideways accelerations. These do not correspond to commensurate changes in body heading, and the insect's flight direction and body heading are decoupled during flight. These findings call in to question the role of yaw control in mosquito flight. In addition, using orientation data, we find that sideways accelerations are well explained by roll-based rotation of the lift vector. In contrast, the insect's body pitch...

  14. A system architecture for long duration free floating flight for military applications

    SciTech Connect (OSTI)

    Epley, L.E. )

    1990-08-31

    Accessibility is today's space frontier. Our need for wide-band global communications, earth imaging an sensing, atmospheric measurements and military reconnaissance is endless but growing dependence on space-based systems raises concerns about potential vulnerability. Military commanders want space assets more accessible and under direct local control. As a result, a robust and low cost access to space-like capability has become a national priority. Buoyant vehicles, free floating in the middle stratosphere could provide the kind of cost effective access to space-like capability needed for a verity of missions. These vehicles are inexpensive, invisible and easily launched. Developments in payload electronics, atmospheric wind modeling and materials combined with ever-improving communications and navigation infrastructure are making balloon-borne concepts more attractive. The fundamental question is whether a free floating balloon, used in a pseudo-satellite role, has value in a military system. Flight tests are ongoing under NASA sponsorship. Following these tests NASA intends to use the vehicles for research in the Antarctic. The concept is being reviewed by other agencies interested in stratospheric research. We believe that LDFFF systems have applications in areas of communications, surveillance and other traditional satellite missions. Dialogue with the broader community of space users is needed to expand the applications. This report reviews the status of the recent flight tests and presents an overview of the concept of Long Duration Free Floating Flight for military applications. 12 refs., 13 figs.

  15. Biomechanics and evolution of flight in stick insects

    E-Print Network [OSTI]

    Zeng, Yu

    2013-01-01

    4 Biomechanics of flight reduction along ecologicalarray experiment . . . 3 The biomechanics of aerial righting35] R. Dudley. The biomechanics of insect flight: form,

  16. Electromagnetic formation flight dipole solution planning

    E-Print Network [OSTI]

    Schweighart, Samuel A. (Samuel Adam), 1977-

    2005-01-01

    Electromagnetic Formation Flight (EMFF) describes the concept of using electromagnets (coupled with reaction wheels) to provide all of the necessary forces and torques needed to maintain a satellite's relative position and ...

  17. Micromechanical actuators for insect flight mechanics

    E-Print Network [OSTI]

    Zhou, Hui, M.S. Massachusetts Institute of Technology

    2008-01-01

    This project aims to develop MEMS actuators to aid in the study of insect flight mechanics. Specifically, we are developing actuators that can stimulate the antennae of the crepuscular hawk moth Manduca Sexta. The possible ...

  18. Autonomous inverted helicopter flight via reinforcement learning

    E-Print Network [OSTI]

    Thrun, Sebastian

    Autonomous inverted helicopter flight via reinforcement learning Andrew Y. Ng 1 , Adam Coates 1 Computer Science Department, Stanford University, Stanford, CA 94305 2 Whirled Air Helicopters, Menlo Park, CA 94025 Abstract. Helicopters have highly stochastic, nonlinear, dynamics, and autonomous helicopter

  19. Parameterized Maneuver Learning for Autonomous Helicopter Flight

    E-Print Network [OSTI]

    O'Brien, James F.

    Parameterized Maneuver Learning for Autonomous Helicopter Flight Jie Tang, Arjun Singh, Nimbus aerobatic maneuvers by our autonomous helicopter. I. INTRODUCTION Trajectory following is a fundamental probabilistic model that enabled them to extract an expert helicopter pilot's intended trajectory from multiple

  20. Autonomous inverted helicopter flight via reinforcement learning

    E-Print Network [OSTI]

    Thrun, Sebastian

    Autonomous inverted helicopter flight via reinforcement learning Andrew Y. Ng1 , Adam Coates1 Science Department, Stanford University, Stanford, CA 94305 2 Whirled Air Helicopters, Menlo Park, CA 94025 Abstract. Helicopters have highly stochastic, nonlinear, dynamics, and autonomous helicopter

  1. Flight at Low Ambient Humidity Increases Protein Catabolism

    E-Print Network [OSTI]

    Zanette, Liana

    and to increase flight range, (ii) the requirement for gluconeogenesis and anaplerosis of Kreb's cycle

  2. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    of Contents Goddard Updates From the Director ­ 2 LaunchFest Rewind ­ 3 A 2008 Photo Gallery ­ 4 2008 Mission: Visitors and Goddard employees alike enjoy LaunchFest. Photo credit: Debora McCallum. GoddardView Info. We provide critical support to manned missions and develop technology that improves everyday life

  3. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    to GLAST Pg 9 Satellites Illuminate Pollution's Influence On Clouds Pg 10 #12;GoddardView Volume 4, Issue 9 Satellites Illuminate Pollution's Influence On Clouds ­ 10 Goddard Family Meet the Faces at Goddard Behind with which she works closely, including NOAA and the Air Force Weather Agency. She is an active participant

  4. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    Diversity Through Art Pg 11 #12;GoddardView Volume 1 Issue 7 October 2005 Table of Contents Inside Week - 10 Goddard Diversity Exploring Diversity Through Art - 11 Goddard Family Employee Spotlight - 12 submit contribu- tions to the editor via e-mail at alittle@pop100.gsfc.nasa.gov. Ideas for new stories

  5. P12A.8 NASA GPM/PMM PARTICIPATION IN THE CANADIAN CLOUDSAT/CALIPSO VALIDATION PROJECT (C3VP): PHYSICAL PROCESS STUDIES IN SNOW

    E-Print Network [OSTI]

    Rutledge, Steven

    P12A.8 NASA GPM/PMM PARTICIPATION IN THE CANADIAN CLOUDSAT/CALIPSO VALIDATION PROJECT (C3VP Univ. Maryland Baltimore County 6 NASA Wallops Flight Facility 7 Dept. of Atmospheric Science, Colorado State University 8 NASA Goddard Space Flight Center 1. INTRODUCTION * A complete understanding

  6. The Space of Metric Spaces

    E-Print Network [OSTI]

    *D. J. Kelleher

    2013-11-16

    The Space of Metric Spaces. *D. J. Kelleher1. 1Department of Mathematics. University of Connecticut. UConn— SIGMA Seminar — Fall 2013. D. J. Kelleher.

  7. Physics Results From Alpha Magnetic Spectrometer 1998 Shuttle Flight

    E-Print Network [OSTI]

    Ming-Huey A. Huang

    2001-04-13

    The Alpha Magnetic Spectrometer (AMS) is a particle detector designed to detect antimatter. During the 10-day test flight on the space shuttle in June 1998, AMS detected $10^8$ events. Upon analysis, no antimatter was found and the antimatter limit was reduced to $1.1\\times10^{-6}$. The proton spectrum shows some differences with the cosmic ray flux used in atmospheric neutrino simulation. A large amount of protons, positrons, and electrons were found below the geomagnetic rigidity cutoff. The energy of these particles are as high as several GeV, one order of magnitude higher than any previously measured energy in radiation belts. These particles also exhibit many interesting features. This paper reviews the results in the four published papers of the AMS collaboration and provides explanation for some features of the albedo particles.

  8. Engineering the Zero-Point Field and Polarizable Vacuum For Interstellar Flight

    E-Print Network [OSTI]

    H. E. Puthoff; S. R. Little

    2010-12-23

    A theme that has come to the fore in advanced planning for long-range space exploration is the concept of "propellantless propulsion" or "field propulsion." One version of this concept involves the projected possibility that empty space itself (the quantum vacuum, or space-time metric) might be manipulated so as to provide energy/thrust for future space vehicles. Although such a proposal has a certain science-fiction quality about it, modern theory describes the vacuum as a polarizable medium that sustains energetic quantum fluctuations. Thus the possibility that matter/vacuum interactions might be engineered for space-flight applications is not a priori ruled out, although certain constraints need to be acknowledged. The structure and implications of such a far-reaching hypothesis are considered herein.

  9. Management and planning of UAV flight pattern

    E-Print Network [OSTI]

    Management and planning of UAV flight pattern Pre-conference Tutorial on Unmanned Aerial Vehicle in Geomatics ETH Zurich, 13/09/11 Magali Barbier UAV-g 2011 ­ Pre-conference Tutorial, Zurich, 13/09/112 Outline · Context: UAV, mission, autonomy, architecture · Experimental means · Application 1: visual

  10. "FLIGHT PLAN" FORECASTS SEATTLE/TACOMA AND

    E-Print Network [OSTI]

    ASSESSMENT OF THE "FLIGHT PLAN" FORECASTS FOR SEATTLE/TACOMA AND REGIONAL AIRPORTS TOGETHER 1. Introduction 5 2. Airport Planning Process 7 Traditional Master Planning Application to Seattle/Tacoma. Uncertainty about Capacity 27 A Fuzzy Concept Assessment Factors Application to Seattle/Tacoma 7. Assessment

  11. Gliding and the Functional Origins of Flight

    E-Print Network [OSTI]

    McGuire, Jimmy A.

    in terrestrial vertebrates suggests progression within an arboreal context from jumping to directed aerial pathways involved in flight evolution. 179 Annu.Rev.Ecol.Evol.Syst.2007.38:179-201.Downloadedfromarjournals transitions, such as those between aquatic and terrestrial environments or between land and air, represent

  12. Space Kimchi

    E-Print Network [OSTI]

    Hacker, Randi; Oborny, Jaimie; Tsutsui, William

    2006-07-05

    Broadcast Transcript: In space, no one can hear you scream... but did you know that in space no one can detect your smell either? The smell-taste connection means that food in space is not only weightless but tasteless, too. What's a flavor...

  13. Systems integration and upgrade of an Engineering Flight Simulator 

    E-Print Network [OSTI]

    Alcorn, William Pleasant

    2002-01-01

    This thesis presents the system integration and upgrade of the Texas A&M Flight Mechanics Laboratory Engineering Flight Simulator (EFS). This upgrade replaced the previous EFS, a simplistic design that did not resemble an aircraft cockpit...

  14. Master of Science Thesis Design, implementation and flight

    E-Print Network [OSTI]

    Langendoen, Koen

    Master of Science Thesis Design, implementation and flight test of indoor navigation and control and flight test of indoor navigation and control system for a quadrotor UAV Master of Science Thesis and flight test of indoor navigation and control system for a quadrotor UAV" by Menno Wierema B

  15. Amazing Cells Fight or Flight Response: Play-by-Play

    E-Print Network [OSTI]

    Clayton, Dale H.

    Module Amazing Cells Fight or Flight Response: Play-by-Play © 2008 University of Utah This document of the most remarkable examples of cell communication is the fight or flight response. When a threat occurs situations. The movie depicts just some of the communication and responses involved in the fight or flight

  16. National Aeronautics and Space Administration goddardviewVolume 7 Issue 7

    E-Print Network [OSTI]

    Christian, Eric

    Telescope's primary mirror segments are prepped to begin final cryogenic testing at Marshall Space Flight observations with the COS instrument), and NASA's Chandra (X-ray) Observatory and Swift (gamma-ray) satellites

  17. American Institute of Aeronautics and Astronautics The Future of Asset Management for Human Space

    E-Print Network [OSTI]

    de Weck, Olivier L.

    American Institute of Aeronautics and Astronautics 1 The Future of Asset Management for Human Space Pasadena, CA 91109 One of the major logistical challenges in human space exploration is asset management. This paper presents observations on the practice of asset management in support of human space flight to date

  18. American Institute of Aeronautics and Astronautics Space Logistics Modeling and Simulation Analysis using

    E-Print Network [OSTI]

    de Weck, Olivier L.

    American Institute of Aeronautics and Astronautics 1 Space Logistics Modeling and Simulation at the International Space Station in low-Earth orbit, logistics is complicated by flights arriving from five launch sites on Earth. The future challenges of space logistics given complex campaigns of interconnected

  19. On the flight of an American Football

    E-Print Network [OSTI]

    Curtis Horn; Heidi Fearn

    2007-06-04

    In this paper we examine the detailed theory of the American football in flight, with spin and air resistance included. We find the theory has much in common with the theory of a gyroscope and also rocket trajectory with a misaligned thruster. Unfortunately most of the air resistance data, for rocketry and ballistics, is for speeds of Mach 1 or higher, where the air resistance increases dramatically. We shall approximate a realistic air resistance, at the slower speeds of football flight, with a drag force proportional to cross sectional area and either $v$ or $v^2$, depending on speed, where $v$ is velocity of the football. We begin with a discussion of the motion, giving as much detail as possible without the use of complex analytic calculations. We point out the previous errors made with moments of inertia and make the necessary corrections for more accurate results. We show that the shape of an American football closely resembles a parabola of revolution.

  20. On the flight of an American Football

    E-Print Network [OSTI]

    Horn, Curtis

    2007-01-01

    In this paper we examine the detailed theory of the American football in flight, with spin and air resistance included. We find the theory has much in common with the theory of a gyroscope and also rocket trajectory with a misaligned thruster. Unfortunately most of the air resistance data, for rocketry and ballistics, is for speeds of Mach 1 or higher, where the air resistance increases dramatically. We shall approximate a realistic air resistance, at the slower speeds of football flight, with a drag force proportional to cross sectional area and either $v$ or $v^2$, depending on speed, where $v$ is velocity of the football. We begin with a discussion of the motion, giving as much detail as possible without the use of complex analytic calculations. We point out the previous errors made with moments of inertia and make the necessary corrections for more accurate results. We show that the shape of an American football closely resembles a parabola of revolution.

  1. Los Alamos Novel Rocket Design Flight Tested

    SciTech Connect (OSTI)

    Tappan, Bryce

    2014-10-23

    Los Alamos National Laboratory scientists recently flight tested a new rocket design that includes a high-energy fuel and a motor design that also delivers a high degree of safety. Researchers will now work to scale-up the design, as well as explore miniaturization of the system, in order to exploit all potential applications that would require high-energy, high-velocity, and correspondingly high safety margins.

  2. Los Alamos Novel Rocket Design Flight Tested

    ScienceCinema (OSTI)

    Tappan, Bryce

    2015-01-05

    Los Alamos National Laboratory scientists recently flight tested a new rocket design that includes a high-energy fuel and a motor design that also delivers a high degree of safety. Researchers will now work to scale-up the design, as well as explore miniaturization of the system, in order to exploit all potential applications that would require high-energy, high-velocity, and correspondingly high safety margins.

  3. High-alpha space trucks

    SciTech Connect (OSTI)

    Cook, L.M. [Ball Aerospace and Technology Corp. 1600 Commerce St. MS CO-9 Boulder, Colorado80301 (United States); Ball, J. [McDonnel Douglas Aerospace 5301 Bolsa Ave. MS 13-3 Huntington Beach, California92647 (United States)

    1997-01-01

    Vertically-landing Reusable Launch Vehicles (RLVs) are the best hope of building a true {open_quotes}Space Truck{close_quotes} with current technology. Because they do not require a low angle-of-attack (AOA, or alpha) horizontal landing, they can be designed to operate exclusively at very high angles-of-attack. This offers savings in vehicle dry weight and complexity, which can be traded for significantly heavier payload, more ascent velocity, or extra design margin. The price for abandoning low angle-of-attack flight is reduced crossrange. To quantify the potential weight reduction, a trade study was performed to determine the relationship between a vehicle{close_quote}s maximum crossrange (angle-of-attack) and it{close_quote}s dry weight (payload margin). At the study conclusion, three vertically-landing (VL) vehicles provided multiple points on a payload weight vs. maximum crossrange curve, showing significant payload increases as crossrange is sacrificed. This is primarily the result of being able to simplify the structure, fly a cooler entry trajectory, and be aerodynamically stable through the entire flight. This reduces subsystem requirements and complexity, enhancing reliability. Further benefits are realized in reduced landing propellant requirements and simplifying or eliminating the {open_quotes}rotation{close_quotes} maneuver. This paper also suggests unique operability solutions that adapt high-alpha vehicles to traditional high-crossrange missions such as the polar {open_quotes}once-around{close_quotes} flight, and proposes a small scale drop-test program to prove the subsonic and landing portion of the flight envelope. {copyright} {ital 1997 American Institute of Physics.}

  4. Aging Enhances Indirect Flight Muscle Fiber Performance yet Decreases Flight Ability in Drosophila

    SciTech Connect (OSTI)

    Miller, Mark S.; Lekkas, Panagiotis; Braddock, Joan M.; Farman, Gerrie P.; Ballif, Bryan A.; Irving, Thomas C.; Maughan, David W.; Vigoreaux, Jim O. (IIT); (Vermont)

    2008-10-02

    We investigated the effects of aging on Drosophila melanogaster indirect flight muscle from the whole organism to the actomyosin cross-bridge. Median-aged (49-day-old) flies were flight impaired, had normal myofilament number and packing, barely longer sarcomeres, and slight mitochondrial deterioration compared with young (3-day-old) flies. Old (56-day-old) flies were unable to beat their wings, had deteriorated ultrastructure with severe mitochondrial damage, and their skinned fibers failed to activate with calcium. Small-amplitude sinusoidal length perturbation analysis showed median-aged indirect flight muscle fibers developed greater than twice the isometric force and power output of young fibers, yet cross-bridge kinetics were similar. Large increases in elastic and viscous moduli amplitude under active, passive, and rigor conditions suggest that median-aged fibers become stiffer longitudinally. Small-angle x-ray diffraction indicates that myosin heads move increasingly toward the thin filament with age, accounting for the increased transverse stiffness via cross-bridge formation. We propose that the observed protein composition changes in the connecting filaments, which anchor the thick filaments to the Z-disk, produce compensatory increases in longitudinal stiffness, isometric tension, power and actomyosin interaction in aging indirect flight muscle. We also speculate that a lack of MgATP due to damaged mitochondria accounts for the decreased flight performance.

  5. Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER)

    E-Print Network [OSTI]

    and Space Administration Goddard Space Flight Center Jet Propulsion Laboratory San Francisco Bay Region region. The com- bination of bands portrays vegetation in red, and urban areas in gray. Sediment of the spectrum, because it's here that almost 100% of the sun's energy reaches the surface. In con- trast, due

  6. www.elsevier.com/locate/asr Available online at www.sciencedirect.com

    E-Print Network [OSTI]

    Cummer, Steven A.

    , Durham, NC 27708, USA `Space Science Data Operations Ofice, NASA Goddard Space Flight Center, Greenbelt instruments were the WAVES instrument on WIND and the WBD instrument on CLUSTER. These experiments showed electron density and magnetic field is a powerful tech- nique with unique, large-scale measurement

  7. Combined distance-of-flight and time-of-flight mass spectrometer

    DOE Patents [OSTI]

    Enke, Christie G; Ray, Steven J; Graham, Alexander W; Hieftje, Gary M; Barinaga, Charles J; Koppenaal, David W

    2014-02-11

    A combined distance-of-flight mass spectrometry (DOFMS) and time-of-flight mass spectrometry (TOFMS) instrument includes an ion source configured to produce ions having varying mass-to-charge ratios, a first detector configured to determine when each of the ions travels a predetermined distance, a second detector configured to determine how far each of the ions travels in a predetermined time, and a detector extraction region operable to direct portions of the ions either to the first detector or to the second detector.

  8. Flight Without Horizon References in European Starlings

    E-Print Network [OSTI]

    Moyle, Robert G.; Heppner, Frank H.

    1998-07-01

    :16:41 PM All use subject to JSTOR Terms and Conditions 772 Short Communications [Auk, Vol. 115 Plexiglas. Rayner (1994) summarized previous wind- tunnel studies and described how free flight may dif- fer from that in a closed-section wind tunnel. Wild... and navigation: A symposium. NASA SP- 262. United States Government Printing Office, Washington, D.C. JANDER, R. 1975. Ecological aspects of spatial orien- tation. Annual Review of Ecology and System- atics 6:171-188. RAYNER, J. M. V. 1994. Aerodynamic...

  9. Argonne In-Flight Radioactive Ion Separator

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room News Publications TraditionalWithAntiferromagnetic SpinsSolicitationsLaboratoryIn-Flight

  10. Flight Path 30R - About ICE II

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home Room NewsInformation Current HABFES OctoberEvanServices »First ObservationFast ThisAboutR° flight

  11. Flight Path Target 4 East Port

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of NaturalDukeWakefieldSulfateSciTechtail.Theory ofDid you not find whatGasEnergyfeature photoTheory05 Target 1 Flight

  12. The Flight Paths for Biojet Fuel

    Gasoline and Diesel Fuel Update (EIA)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity of Natural GasAdjustments (Billion Cubic Feet) Wyoming963 1.969 1.979 1.988Prices,Flight Paths for Biojet Fuel Tony Radich

  13. Flight Test of Weapons System Body by Navy Successful | National...

    National Nuclear Security Administration (NNSA)

    nuclear explosive testing." The FCET-51 reentry body was designed to measure vibration and shock environments in flight. The next-generation telemetry capability was...

  14. The Astrophysical Journal, 718:331339, 2010 July 20 doi:10.1088/0004-637X/718/1/331 C 2010. The American Astronomical Society. All rights reserved. Printed in the U.S.A.

    E-Print Network [OSTI]

    Gelbord, Jonathan

    , VP62, NASA/Marshall Space Flight Center, Huntsville, AL 35812, USA 5 NASA/Goddard Space Flight Center; published 2010 June 30 ABSTRACT On 2010 March 19, the Swift/Burst Alert Telescope triggered on a short burst with the Swift/X-Ray Telescope and the Rossi X-ray Timing Explorer led to the discovery of a new X-ray source

  15. National Aeronautics and Space Administration www.nasa.gov

    E-Print Network [OSTI]

    Christian, Eric

    National Aeronautics and Space Administration www.nasa.gov Volume 10 Issue 8 July 2014 #12;A multitude of NASA research investigations, crew provisions, hardware and science experiments from across. The cargo craft launched aboard Orbital's An- tares rocket from NASA's Wallops Flight Facility in Virginia

  16. Note: A novel dual-channel time-of-flight mass spectrometer for photoelectron imaging spectroscopy

    SciTech Connect (OSTI)

    Qin Zhengbo; Wu Xia; Tang Zichao [State Key Laboratory of Molecular Reaction Dynamics, Dalian Institute of Chemical Physics, Chinese Academy of Sciences, Dalian 116023 (China)

    2013-06-15

    A novel dual-channel time-of-flight mass spectrometer (D-TOFMS) has been designed to select anions in the photoelectron imaging measurements. In this instrument, the radiation laser can be triggered precisely to overlap with the selected ion cloud at the first-order space focusing plane. Compared with that of the conventional single channel TOFMS, the in situ mass selection performance of D-TOFMS is significantly improved. Preliminary experiment results are presented for the mass-selected photodetachment spectrum of F{sup -} to demonstrate the capability of the instrument.

  17. LMS Qualification and Flight Acceptance T /V Test Summary

    E-Print Network [OSTI]

    Rathbun, Julie A.

    LMS Qualification and Flight Acceptance T /V Test Summary and Thermal Design Final Report NO. ATMIIIIDe yablinaDhllalan LMS Qualification and Flight Acceptance T/V Test Summary and Thermal Design Final Report PAGI DATI SUMMARY The LMS maintains thermal control. within the -10 to +125°F operating temperature

  18. An Application of Reinforcement Learning to Aerobatic Helicopter Flight

    E-Print Network [OSTI]

    Thrun, Sebastian

    An Application of Reinforcement Learning to Aerobatic Helicopter Flight Pieter Abbeel, Adam Coates Autonomous helicopter flight is widely regarded to be a highly challenging control problem. This paper presents the first successful autonomous completion on a real RC helicopter of the following four aerobatic

  19. Prediction of Jet Noise Shielding with Forward Flight Salvador Mayoral

    E-Print Network [OSTI]

    Papamoschou, Dimitri

    Prediction of Jet Noise Shielding with Forward Flight Effects Salvador Mayoral and Dimitri on the radiation of the isolated source as well as its diffraction by an object. Applications include the shielding to better shielding for the HWB problem. The overall error tends to be less than 5% for flight Mach number

  20. Adaptive control for Mars atmospheric flight 

    E-Print Network [OSTI]

    Restrepo, Carolina Isabel

    2009-05-15

    The new vision for space exploration will focus on sending humans to the moon and eventually to Mars. This endeavor presents new challenges that are critically di?erent from the past experience with robotic missions to ...

  1. Cosmic-Ray Studies with an Alpha Magnetic Spectrometer (AMS Detector) on the International Space Station

    SciTech Connect (OSTI)

    Plyaskin, V.V. [Institute of Theoretical and Experimental Physics, Bol'shaya Cheremushkinskaya ul. 25, Moscow, 117259 (Russian Federation)

    2005-01-01

    A brief description of the physics research program implemented with an alpha magnetic spectrometer (AMS detector) by a large-scale international collaboration on board the International Space Station is presented. The features of the experimental facility under construction are given, along with some results obtained during the test flight of the prototype spectrometer on board a space shuttle.

  2. Human-Robotic Cooperative Teams for Advanced Space Operations David L. Akin

    E-Print Network [OSTI]

    Akin, David

    1 Human-Robotic Cooperative Teams for Advanced Space Operations David L. Akin Abstract Flight and research experience to date indicates that teams of robots and humans will provide significantly greater in the University of Maryland Space Systems Laboratory on three different approaches to human/robotic interaction

  3. Genetic algorithms for tuning fuzzy membership functions in flight control software 

    E-Print Network [OSTI]

    Harral, Vance Quinton

    1995-01-01

    to their general aviation brethren. One project developed during the course of this research was a Flight Mode Interpreter (FMI). The FMI performs real-time, high-level situation recognition based on data from aircraft flight instruments. Flight modes...

  4. A comparison of four direct geometry time-of-flight spectrometers at the Spallation Neutron Source

    SciTech Connect (OSTI)

    Stone, Matthew B [ORNL; Niedziela, Jennifer L [ORNL; Abernathy, Douglas L [ORNL; Debeer-Schmitt, Lisa M [ORNL; Garlea, Vasile O [ORNL; Granroth, Garrett E [ORNL; Graves-Brook, Melissa K [ORNL; Ehlers, Georg [ORNL; Kolesnikov, Alexander I [ORNL; Podlesnyak, Andrey A [ORNL; Winn, Barry L [ORNL

    2014-04-01

    The Spallation Neutron Source at Oak Ridge National Laboratory now hosts four direct geometry time-of-flight chopper spectrometers. These instruments cover a range of wave vector and energy transfer space with varying degrees of neutron flux and resolution. The regions of reciprocal and energy space available to measure at these instruments is not exclusive and overlaps significantly. We present a direct comparison of the capabilities of this instrumentation, conducted by data mining the instrument usage histories, and specific scanning regimes. In addition, one of the common science missions for these instruments is the study of magnetic excitations in condensed matter systems. We have measured the powder averaged spin wave spectra in one particular sample using each of these instruments, and use these data in our comparisons.

  5. A comparison of four direct geometry time-of-flight spectrometers at the Spallation Neutron Source

    SciTech Connect (OSTI)

    Stone, M. B.; Abernathy, D. L.; Ehlers, G.; Garlea, O.; Podlesnyak, A.; Winn, B. [Quantum Condensed Matter Science Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States)] [Quantum Condensed Matter Science Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States); Niedziela, J. L.; DeBeer-Schmitt, L.; Graves-Brook, M. [Instrument and Source Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States)] [Instrument and Source Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States); Granroth, G. E. [Neutron Data Analysis and Visualization Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States)] [Neutron Data Analysis and Visualization Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States); Kolesnikov, A. I. [Chemical and Engineering Materials Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States)] [Chemical and Engineering Materials Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States)

    2014-04-15

    The Spallation Neutron Source at Oak Ridge National Laboratory now hosts four direct geometry time-of-flight chopper spectrometers. These instruments cover a range of wave-vector and energy transfer space with varying degrees of neutron flux and resolution. The regions of reciprocal and energy space available to measure at these instruments are not exclusive and overlap significantly. We present a direct comparison of the capabilities of this instrumentation, conducted by data mining the instrument usage histories, and specific scanning regimes. In addition, one of the common science missions for these instruments is the study of magnetic excitations in condensed matter systems. We have measured the powder averaged spin wave spectra in one particular sample using each of these instruments, and use these data in our comparisons.

  6. U.S. Department of Commerce National Oceanic and Atmospheric Administration

    E-Print Network [OSTI]

    Center (SSMC) Building 1 and Building 3. NOAA5006 provides the Local Area Network (LAN) for NESDIS in the Aerospace building and GreenTec4 [GT4] building of the NASA Goddard Space Flight Center (GSFC). The purpose automation support for the programs, offices, and staff of: · Office of Chief Information Officer

  7. Urban aerosols and their variations with clouds and rainfall: A case study for New York and Houston

    E-Print Network [OSTI]

    Jin, Menglin

    warming (urban heat island effect (UHI)) and urban pollution impacts on surface energy budget have raisedUrban aerosols and their variations with clouds and rainfall: A case study for New York and Houston Shepherd Laboratory for Atmospheres, NASA Goddard Space Flight Center, Greenbelt, Maryland, USA Michael D

  8. The consequences of urban land transformation on net primary productivity in the United States

    E-Print Network [OSTI]

    Vermont, University of

    regions. In terms of biologically available energy, the loss of NPP due to urbanization of agriculturalThe consequences of urban land transformation on net primary productivity in the United States Marc , Compton J. Tuckera , Taylor Rickettse a Biospheric Sciences Branch, Code 923, NASA's Goddard Space Flight

  9. AIRBORNE HIGH SPECTRAL RESOLUTION LIDAR AEROSOL MEASUREMENTS DURING CALNEX AND CARES

    E-Print Network [OSTI]

    , and Evgueni Kassianov, Pacific Northwest National Laboratory Brent Holben, NASA Goddard Space Flight Center National Laboratory U.S. Department of Energy Office of Science ABSTRACT The NASA Langley Research Center layers of dust, likely transported from Asia, were located above urban aerosols. HSRL and ground- based

  10. Paranicas et al.: Europa's Radiation Environment 529 Europa's Radiation Environment and Its Effects on the Surface

    E-Print Network [OSTI]

    Johnson, Robert E.

    Paranicas et al.: Europa's Radiation Environment 529 529 Europa's Radiation Environment and Its of Technology R. E. Johnson University of Virginia S. J. Sturner NASA Goddard Space Flight Center and University of Maryland Baltimore County Europa's orbit in the radiation environment of Jupiter is reviewed

  11. Lunar interior properties from the GRAIL mission James G. Williams1

    E-Print Network [OSTI]

    Nimmo, Francis

    Lunar interior properties from the GRAIL mission James G. Williams1 , Alexander S. Konopliv1 , Dale Recovery and Interior Laboratory (GRAIL) mission has sampled lunar gravity with unprecedented accuracy GRAIL Primary Mission data at the Jet Propulsion Laboratory and the Goddard Space Flight Center. The two

  12. MEASUREMENT OF THE POSITRON AND ELECTRON SPECTRA WITH THE CAPRICE EXPERIMENT

    E-Print Network [OSTI]

    Morselli, Aldo

    INFN, Frascati, Italy, 5 NASA/Goddard Space Flight Center, Greenbelt, Maryland, USA, 6 New Mexico State University, Las Cruces, New Mexico, USA, 7 Dipartimento di Fisica dell'Universit`a and Sezione INFN di useful information about solar wind effects on the cosmic rays. Most of the recent measurements

  13. The Astrophysical Journal, 727:132 (9pp), 2011 February 1 doi:10.1088/0004-637X/727/2/132 C 2011. The American Astronomical Society. All rights reserved. Printed in the U.S.A.

    E-Print Network [OSTI]

    Zhang, Bing

    100418A F. E. Marshall1 , L. A. Antonelli2 , D. N. Burrows3 , S. Covino4,5 , M. de Pasquale6 , P. A Science Division, NASA Goddard Space Flight Center, Greenbelt, 20771 MD, USA; frank.marshall@nasa.gov 2.6235 discovered with the Swift Gamma-ray Burst Explorer with unusual optical and X-ray light curves. After

  14. A MEASUREMENT OF THE PROTON SPECTRUM AT 1 AU NEAR SOLAR MINIMUM WITH THE CAPRICE EXPERIMENT

    E-Print Network [OSTI]

    Morselli, Aldo

    OG 5.2.1 A MEASUREMENT OF THE PROTON SPECTRUM AT 1 AU NEAR SOLAR MINIMUM WITH THE CAPRICELaboratori Nazionali INFN, Frascati, Italy 5NASA/Goddard Space Flight Center, Greenbelt, USA 6New Mexico the production and acceleration mechanism of cosmic rays, as well as the solar modulation effect

  15. Four-Field Equations: a New Model for Weakly Compressible MHD... http://flux.aps.org/meetings/YR98/BAPSDPP98/abs/S2500016.html 1 of 1 3/10/05 11:08 AM

    E-Print Network [OSTI]

    Ng, Chung-Sang

    Compressible MHD Turbulence in the Solar Wind and the Interstellar Medium S. Spangler, A. Bhattacharjee, C. S Goddard Space Flight Center) Turbulent plasmas in the solar wind and the interstellar medium often contain are compared with solar wind data from Helios 1 and 2, and found to account qualitatively for the scaling range

  16. From Measurements to Models: What Satellite and Sub-Orbital Instruments

    E-Print Network [OSTI]

    uncertainty upper bounds for ~1 W/m2 TOA DARF accuracy: ~ 0.02 CCSP - SAP 2.3, 2009 #12;Aerosol-location time series Regional Context R. Kahn #12;The NASA Earth Observing System's Terra Satellite ASTER First Light: February 24, 2000 MODIS CERES MISR MOPITT Terra Project Office / NASA Goddard Space Flight Center

  17. THE ASTROPHYSICAL JOURNAL, 565:280296, 2002 January 20 ( 2002. The American Astronomical Society. All rights reserved. Printed in U.S.A.

    E-Print Network [OSTI]

    Moskalenko, Igor V.

    , Postfach 1603, D-85740 Garching, Germany;fu r aws=mpe.mpg.de JONATHAN F. ORMES NASA Goddard Space Flight calculation of the secondary antiproton Ă?ux provides a "" background ĂŹĂŹ for searches for exotic signals from such tests to be performed. We use our propagation code GALPROP to calculate interstellar cosmic

  18. DIFFUSE GALACTIC CONTINUUM GAMMA RAYS: A MODEL COMPATIBLE WITH EGRET DATA AND COSMIC-RAY MEASUREMENTS

    E-Print Network [OSTI]

    Moskalenko, Igor V.

    Garching, Germany; aws@mpe.mpg.de Igor V. Moskalenko1 NASA Goddard Space Flight Center, Code 661, Greenbelt. In particular, the spectrum of -rays calculated under the assumption that the proton and electron spectra -production in p-p interactions. However, a calculation made using modern Monte Carlo event generators

  19. Submillimeter Polarimetry and the Galactic Center Magnetic Field

    E-Print Network [OSTI]

    Novak, Giles

    Submillimeter Polarimetry and the Galactic Center Magnetic Field D.T. Chuss NASA Goddard Space Flight Center C.D. Dowell Jet Propulsion Laboratory R.H. Hildebrand University of Chicago G. Novak that of the magnetic field. In addition, we present new Hertz data on the Dust Ridge, an arched structure

  20. OBSERVATIONS OF PLASMA WAVES NEAR MARS AND THEIR IMPLICATIONS FOR ATMOSPHERIC LOSS. J. R. Espley1

    E-Print Network [OSTI]

    California at Berkeley, University of

    NASA Goddard Space Flight Center, Greenbelt, MD Summary: We use data from over 500 pre- mapping orbits (and therefore climate change). We present in this work observations of magnetic oscillations of Mars Global Surveyor magnetome- ter data to present statistical results on the characteris- tics

  1. Hyperspectral Aerosol Optical Depths from TCAP Flights

    SciTech Connect (OSTI)

    Shinozuka, Yohei; Johnson, Roy R.; Flynn, Connor J.; Russell, P. B.; Schmid, Beat; Redemann, Jens; Dunagan, Stephen; Kluzek, Celine D.; Hubbe, John M.; Segal-Rosenheimer, Michal; Livingston, J. M.; Eck, T.; Wagener, Richard; Gregory, L.; Chand, Duli; Berg, Larry K.; Rogers, Ray; Ferrare, R. A.; Hair, John; Hostetler, Chris A.; Burton, S. P.

    2013-11-13

    4STAR (Spectrometer for Sky-Scanning, Sun-Tracking Atmospheric Research), the world’s first hyperspectral airborne tracking sunphotometer, acquired aerosol optical depths (AOD) at 1 Hz during all July 2012 flights of the Two Column Aerosol Project (TCAP). Root-mean square differences from AERONET ground-based observations were 0.01 at wavelengths between 500-1020 nm, 0.02 at 380 and 1640 nm and 0.03 at 440 nm in four clear-sky fly-over events, and similar in ground side-by-side comparisons. Changes in the above-aircraft AOD across 3-km-deep spirals were typically consistent with integrals of coincident in situ (on DOE Gulfstream 1 with 4STAR) and lidar (on NASA B200) extinction measurements within 0.01, 0.03, 0.01, 0.02, 0.02, 0.02 at 355, 450, 532, 550, 700, 1064 nm, respectively, despite atmospheric variations and combined measurement uncertainties. Finer vertical differentials of the 4STAR measurements matched the in situ ambient extinction profile within 14% for one homogeneous column. For the AOD observed between 350-1660 nm, excluding strong water vapor and oxygen absorption bands, estimated uncertainties were ~0.01 and dominated by (then) unpredictable throughput changes, up to +/-0.8%, of the fiber optic rotary joint. The favorable intercomparisons herald 4STAR’s spatially-resolved high-frequency hyperspectral products as a reliable tool for climate studies and satellite validation.

  2. Particle detection technology for space-borne astroparticle experiments

    E-Print Network [OSTI]

    Martin Pohl

    2014-09-05

    I review the transfer of technology from accelerator-based equipment to space-borne astroparticle detectors. Requirements for detection, identification and measurement of ions, electrons and photons in space are recalled. The additional requirements and restrictions imposed by the launch process in manned and unmanned space flight, as well as by the hostile environment in orbit, are analyzed. Technology readiness criteria and risk mitigation strategies are reviewed. Recent examples are given of missions and instruments in orbit, under construction or in the planning phase.

  3. SPACE DAILY SPACE WAR TERRA DAILY MARS DAILY SPACE MART SPACE TRAVEL World's Smallest Universal Material

    E-Print Network [OSTI]

    Espinosa, Horacio D.

    SPACE DAILY SPACE WAR TERRA DAILY MARS DAILY SPACE MART SPACE TRAVEL NANO TECH World's Smallest, professor of mechanical Get Our Free Newsletters Via Email Space - War - Earth - Energy - China your email yes Search All Of Our Sites In One Search SpaceDaily - SpaceWar - TerraDaily Search Horacio D

  4. Test of the Spare Flight Model of UG electronics

    E-Print Network [OSTI]

    Roma "La Sapienza", Universitŕ di

    Test of the Spare Flight Model of UG electronics for the AMS TRD Gas System Bruno Borgia 1.1 The UG-crate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 1.2 Test setup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 1.3 Functionality test sequence . . . . . . . . . . . . . . . . . . . . . . . . 7 2 FS

  5. Test of the Flight Model of UG electronics

    E-Print Network [OSTI]

    Roma "La Sapienza", Universitŕ di

    Test of the Flight Model of UG electronics for the AMS TRD Gas System Bruno Borgia, Alessandro-crate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 1.2 Test setup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 1.3 Functionality test sequence . . . . . . . . . . . . . . . . . . . . . . . . 7 2 FM qualification test 8 2

  6. When Good Ideas Take Flight: Carlsbad Field Office Shows Support...

    Office of Environmental Management (EM)

    DOE Carlsbad Field Office (CBFO) Manager Joe Franco, right, took to the skies in a New Mexico National Guard UH-60 Blackhawk helicopter flight in southeast New Mexico recently. An...

  7. Vision-Aided Inertial Navigation for Flight Control

    E-Print Network [OSTI]

    Johnson, Eric N.

    wu@ae.gatech.edu. Lockheed Martin Assistant Professor of Avionics Integration, Aerospace Engineering from the fusion of this information with inertial and heading measurements. Simulation and flight test

  8. Flight test and evaluation of Omega navigation for general aviation

    E-Print Network [OSTI]

    Hwoschinsky, Peter V.

    1975-01-01

    A seventy hour flight test program was accomplished to determine the suitability and accuracy of a low cost Omega navigation receiver in a general aviation aircraft. An analysis was made of signal availability in two widely ...

  9. Decomposing global light transport using time of flight imaging

    E-Print Network [OSTI]

    Wu, Di

    Global light transport is composed of direct and indirect components. In this paper, we take the first steps toward analyzing light transport using high temporal resolution information via time of flight (ToF) images. The ...

  10. Lyapunov functions nonlinear spaces

    E-Print Network [OSTI]

    Hafstein, Sigurđur Freyr

    Lyapunov functions on nonlinear spaces R. Sepulchre -- University of Liege, Belgium Reykjavik - July 2013 Constructing Lyapunov functions: a personal journey · Lyap functions in linear spaces (1994: homogeneous spaces with flat, positive, and negative curvature) Lyapunov functions in linear spaces 3

  11. Flying on Sun Shine: Sailing in Space

    SciTech Connect (OSTI)

    Alhorn, Dean

    2012-03-28

    On January 20th, 2011, NanoSail-D successfully deployed its sail in space. It was the first solar sail vehicle to orbit the earth and the second sail ever unfurled in space. The 10m2 sail, deployment mechanism and electronics were packed into a 3U CubeSat with a volume of about 3500cc. The NanoSail-D mission had two objectives: eject a nanosatellite from a minisatellite; deploy its sail from a highly compacted volume to validate large structure deployment and potential de-orbit technologies. NanoSail-D was jointly developed by NASA's Marshall Space Flight Center and Ames Research Center. The ManTech/NeXolve Corporation provided key sail design support. NanoSail-D is managed by Marshall and jointly sponsored by the Army Space and Missile Defense Command, the Space Test Program, the Von Braun Center for Science and Innovation and Dynetics Inc. The presentation will provide insights into sailcraft advances and potential missions enabled by this emerging in-space propulsion technology.

  12. GoddardViewGoddard's 2007 Safety Awareness Campaign Goddard Collaborates with Indigenous People

    E-Print Network [OSTI]

    Christian, Eric

    Delivers Course on Software Engineering - 5 Engineers Become "Composites Designers" as Tiger Team Meets International Polar Year - 3 NASA Detects Trends in Rainfall Traits from Drizzles to Downpours - 4 NESC Academy

  13. Social Media: Space Weather #SpaceWeather

    E-Print Network [OSTI]

    ://www.swpc.noaa.gov/impacts/spaceweatherandgpssystems #SpaceWeather #12;Space Weather Impacts on the Power Grid Facebook The electric power grid. To learn about space weather and impacts to the electric grid visit http on the Power Grid Space Weather and the Aurora Borealis What are Solar Flares? What are Coronal Mass

  14. MAVEN TAkEs FlighT National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Christian, Eric

    's second stage 53 minutes after launch. The solar arrays deployed approximately one hour after launch that is uncovering the mysteries of the solar system and enabling us to reach far- ther destinations." In the next telecommunications relay hardware and operations. n Above: The United Launch Alliance Atlas V rocket lifts off from

  15. THE APPLICATION OF RESILIENCE ENGINEERING TO HUMAN SPACE FLIGHT C.W. Johnson (1)

    E-Print Network [OSTI]

    Johnson, Chris

    that are to be learned after previous incidents. The Inspector General's remit also includes the dissemination of `good, The Netherlands. Fax: +31 71 565 5420, Phone: +31 71 565 3206 ABSTRACT There is a concern that mishap reporting and Close Call Reporting, Investigating, and Recordkeeping (NPR 8621.1B). This document describes

  16. NASA's Marshall Space Flight Center Saves Water with High-Efficiency Toilet

    Energy Savers [EERE]

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on DeliciousMathematicsEnergyInterested Parties -Department of EnergyNEW YORK STATENASA Enhanced Use Leaseand

  17. Software Engineering for Space Exploration Iowa State University and Jet Propulsion Laboratory/California Institute of Technology

    E-Print Network [OSTI]

    Lutz, Robyn R.

    1 Software Engineering for Space Exploration Robyn Lutz Iowa State University and Jet are transforming the way we explore space. Spacecraft are becoming more software-intensive in order to support flight and accelerated understanding of our universe. Advances in software engineering play a vital role

  18. Ultra-wideband radios for time-of-flight-ranging and network position estimation

    DOE Patents [OSTI]

    Hertzog, Claudia A. (Houston, TX); Dowla, Farid U. (Castro Valley, CA); Dallum, Gregory E. (Livermore, CA); Romero, Carlos E. (Livermore, CA)

    2011-06-14

    This invention provides a novel high-accuracy indoor ranging device that uses ultra-wideband (UWB) RF pulsing with low-power and low-cost electronics. A unique of the present invention is that it exploits multiple measurements in time and space for very accurate ranging. The wideband radio signals utilized herein are particularly suited to ranging in harsh RF environments because they allow signal reconstruction in spite of multipath propagation distortion. Furthermore, the ranging and positioning techniques discussed herein directly address many of the known technical challenges encountered in UWB localization regarding synchronization and sampling. In the method developed, noisy, corrupted signals can be recovered by repeating range measurements across a channel, and the distance measurements are combined from many locations surrounding the target in a way that minimizes the range biases associated to indirect flight paths and through-wall propagation delays.

  19. Aircraft Integration and Flight Testing of 4STAR

    SciTech Connect (OSTI)

    Flynn, CJ; Kassianov, E; Russell, P; Redemann, J; Dunagan, S; Holben, B

    2012-10-12

    Under funding from the U.S. Dept. of Energy, in conjunction with a funded NASA 2008 ROSES proposal, with internal support from Battelle Pacific Northwest Division (PNWD), and in collaboration with NASA Ames Research Center, we successfully integrated the Spectrometer for Sky-Scanning, Sun-Tracking Atmospheric Research (4STAR-Air) instrument for flight operation aboard Battelle’s G-1 aircraft and conducted a series of airborne and ground-based intensive measurement campaigns (hereafter referred to as “intensives”) for the purpose of maturing the initial 4STAR-Ground prototype to a flight-ready science-ready configuration.

  20. Normal, Not Paracompact Spaces

    E-Print Network [OSTI]

    Fleissner, William G.

    1982-07-01

    We describe some recently constructed counterexamples in general topology, including a normal, nonmetrizable Moore space, a normal para-Lindelof, not paracompact space, and a normal, screenable, not paracompact space....

  1. Space Solar Power Program

    SciTech Connect (OSTI)

    Arif, H.; Barbosa, H.; Bardet, C.; Baroud, M.; Behar, A.; Berrier, K.; Berthe, P.; Bertrand, R.; Bibyk, I.; Bisson, J.; Bloch, L.; Bobadilla, G.; Bourque, D.; Bush, L.; Carandang, R.; Chiku, T.; Crosby, N.; De Seixas, M.; De Vries, J.; Doll, S.; Dufour, F.; Eckart, P.; Fahey, M.; Fenot, F.; Foeckersperger, S.; Fontaine, J.E.; Fowler, R.; Frey, H.; Fujio, H.; Gasa, J.M.; Gleave, J.; Godoe, J.; Green, I.; Haeberli, R.; Hanada, T.; Ha

    1992-08-01

    Information pertaining to the Space Solar Power Program is presented on energy analysis; markets; overall development plan; organizational plan; environmental and safety issues; power systems; space transportation; space manufacturing, construction, operations; design examples; and finance.

  2. Sculpting space through sound

    E-Print Network [OSTI]

    Nakagawa, Junko, 1975-

    2002-01-01

    How does one experience space? What kind of information do humans collect in the process of constructing space in their mind? How does one begin to understand volume, light, texture, material, smell and sense of space? The ...

  3. INTRODUCTION 1.1 Aerodynamics of Rotors in Forward Flight

    E-Print Network [OSTI]

    design. In order to capture the above physical phenomena, the influence of the inflow, blade dynamics1 CHAPTER I INTRODUCTION 1.1 Aerodynamics of Rotors in Forward Flight The prediction of rotor blade. Shock induced separation and shock motion along the chord of the blade may occur. Because the inboard

  4. Flight Demonstrations of Cooperative Control for UAV Teams

    E-Print Network [OSTI]

    Flight Demonstrations of Cooperative Control for UAV Teams Jonathan How , Ellis King , and Yoshiaki (UAVs) that was designed as a platform for evaluating autonomous coordination and control algorithms. Future UAV teams will have to autonomously demonstrate cooperative behaviors in dynamic and uncertain

  5. A Review on Fish Swimming and Bird/Insect Flight

    E-Print Network [OSTI]

    Theodore Yaotsu Wu

    2010-07-29

    This expository review is devoted to fish swimming and bird/insect flight. (i) The simple waving motion of an elongated flexible ribbon plate of constant width, immersed in a fluid at rest, propagating a wave distally down the plate to swim forward is first considered to provide a fundamental concept on energy conservation. It is generalized to include variations in body width and thickness, vortex shedding from appended dorsal, ventral and caudal fins to closely simulate fish swimming for which a nonlinear theory is presented for large-amplitude propulsion. (ii) For bird flight, the pioneering studies on oscillating rigid wings are briefed, followed by presenting a nonlinear unsteady theory for flexible wing with arbitrary variations in shape and trajectory with a comparative study with experiments. (iii) For insect flight, more recent advances are reviewed under aerodynamic theory and modeling, computational methods, and experiments, on forward and hovering flights with producing leading-edge vortex to give unsteady high lift. (iv) Prospects are explored on extracting intrinsic flow energy by fish and bird to gain thrust for propulsion. (v) The mechanical and biological principles are drawn together for unified studies on the energetics in deriving metabolic power for animal locomotion, leading to a surprising discovery that the hydrodynamic viscous drag on swimming fish is largely associated with laminar boundary layers, thus drawing valid and sound evidences for a resolution to the fish-swim paradox proclaimed by Gray (1936, 1968).

  6. Systematic Verification of Operational Flight Program through Reverse Engineering

    E-Print Network [OSTI]

    project aims to develop an unmanned helicopter and its on-flight embedded computing system for navigation services for unmanned helicopter that shall be used for disaster response or recovery using real and actuators equipped in the helicopter. The OFP as a safety-critical and mission-critical system should

  7. Unsteady Aerodynamic Models for Agile Flight at Low Reynolds Numbers

    E-Print Network [OSTI]

    Rowley, Clarence W.

    for Wagner's and Theodorsen's models, making them compatible with modern control-system analysis. A number thanks are to my advisor, Clancy Rowley, who has been both a role model and a source of encouragementUnsteady Aerodynamic Models for Agile Flight at Low Reynolds Numbers Steven L. Brunton

  8. Chaos in Nonlinear Dynamical Systems Helicopter Flight-data Analysis

    E-Print Network [OSTI]

    Taylor, James H.

    Chaos in Nonlinear Dynamical Systems ­ Helicopter Flight-data Analysis James H. Taylor1 and S of chaos in nonlinear dynamical systems is discussed, and approaches for the identification of chaos can only occur in systems with nonlinear dynamics. The recognition of chaos in a complex dynamical

  9. HOVERING FLIGHT FOR A MICROMECHANICAL FLYING INSECT: MODELING AND ROBUST

    E-Print Network [OSTI]

    California at Berkeley, University of

    Schenato Xinyan Deng Shankar Sastry Department of Electrical Engineering and Computer Sciences recent remarkable achievements obtained with fixed and rotary air- crafts (Shim et al., 2000), their use to aerial vehicles based on rotary wings, such as helicopter, flying insects control their flight

  10. SENSORIMOTOR CONVERGENCE IN VISUAL NAVIGATION AND FLIGHT CONTROL

    E-Print Network [OSTI]

    Murray, Richard M.

    in the processing of retinal image pattern movement (optic flow) by the visuomotor systems of insects, one of na of optic flow are extracted by retinal motion sensitivity kernels. ditional approach, LPTC-based processing processing and convergence of visual sensory information to flight motor commands via spatial wide

  11. Survey of historical incidences with Controls-Structures Interaction and recommended technology improvements needed to put hardware in space

    SciTech Connect (OSTI)

    Ketner, G.L.

    1989-03-01

    Pacific Northwest Laboratory (PNL) conducted a survey for the Controls-Structures Interaction (CSI) Office of the National Aeronautics and Space Administration's (NASA) Langley Research Center. The purpose of the survey was to collect information documenting past incidences of problems with CSI during design, analysis, ground development, test and/or flight operation of space systems in industry. The survey was conducted to also compile recommended improvements in technology to support future needs for putting hardware into space. 3 refs., 1 tab.

  12. The Alpha Magnetic Spectrometer (AMS): search for antimatter and dark matter on the International Space Station

    E-Print Network [OSTI]

    R. Battiston

    1997-08-27

    The AMS is a state of the art detector for extraterrestrial study of antimatter, matter and missing matter. After a precursor flight on STS91 in May 1998, AMS will be installed on the International Space Station where it will operate for three years. In this paper the AMS experiment is described and is physics potential reviewed.

  13. Reaction-in-Flight Neutrons and the Stopping Power in Cryogenic...

    Office of Scientific and Technical Information (OSTI)

    Reaction-in-Flight Neutrons and the Stopping Power in Cryogenic NIF Capsules Citation Details In-Document Search Title: Reaction-in-Flight Neutrons and the Stopping Power in...

  14. The Chandra High Energy Transmission Grating: Design, Fabrication, Ground Calibration and Five Years in Flight

    E-Print Network [OSTI]

    Canizares, Claude R.

    Details of the design, fabrication, and ground and flight calibration of the High Energy Transmission Grating (HETG) on the Chandra X?Ray Observatory are presented after 5 years of flight experience. Specifics include the ...

  15. Cryogenic heat pipe for cooling high temperature superconductors with application to Electromagnetic Formation Flight Satellites

    E-Print Network [OSTI]

    Kwon, Daniel W., 1980-

    2009-01-01

    An emerging method of propellant-less formation flight propulsion is the use of electromagnets coupled with reaction wheels. This technique is called Electromagnetic Formation Flight (EMFF). In order to create a large ...

  16. Design and safety analysis of an in-flight, test airfoil 

    E-Print Network [OSTI]

    McKnight, Christopher William

    2006-10-30

    The evaluation of an in-flight airfoil model requires extensive analysis of a variety of structural systems. Determining the safety of the design is a unique task dependant on the aircraft, flight environment, and physical requirements...

  17. Ongoing Space Nuclear Systems Development in the United States

    SciTech Connect (OSTI)

    S. Bragg-Sitton; J. Werner; S. Johnson; Michael G. Houts; Donald T. Palac; Lee S. Mason; David I. Poston; A. Lou Qualls

    2011-10-01

    Reliable, long-life power systems are required for ambitious space exploration missions. Nuclear power and propulsion options can enable a bold, new set of missions and introduce propulsion capabilities to achieve access to science destinations that are not possible with more conventional systems. Space nuclear power options can be divided into three main categories: radioisotope power for heating or low power applications; fission power systems for non-terrestrial surface application or for spacecraft power; and fission power systems for electric propulsion or direct thermal propulsion. Each of these areas has been investigated in the United States since the 1950s, achieving various stages of development. While some nuclear systems have achieved flight deployment, others continue to be researched today. This paper will provide a brief overview of historical space nuclear programs in the U.S. and will provide a summary of the ongoing space nuclear systems research, development, and deployment in the United States.

  18. Advanced Space Propulsion Based on Vacuum (Spacetime Metric) Engineering

    E-Print Network [OSTI]

    Harold E. Puthoff

    2012-02-03

    A theme that has come to the fore in advanced planning for long-range space exploration is the concept that empty space itself (the quantum vacuum, or spacetime metric) might be engineered so as to provide energy/thrust for future space vehicles. Although far-reaching, such a proposal is solidly grounded in modern physical theory, and therefore the possibility that matter/vacuum interactions might be engineered for space-flight applications is not a priori ruled out. As examples, the current development of theoretical physics addresses such topics as warp drives, traversable wormholes and time machines that provide for such vacuum engineering possibilities. We provide here from a broad perspective the physics and correlates/consequences of the engineering of the spacetime metric.

  19. Thick-to-Thin Filament Surface Distance Modulates Cross-Bridge Kinetics in Drosophila Flight Muscle

    SciTech Connect (OSTI)

    Tanner, Bertrand C.W.; Farman, Gerrie P.; Irving, Thomas C.; Maughan, David W.; Palmer, Bradley M.; Miller, Mark S. (IIT); (Vermont); (BU)

    2012-09-19

    The demembranated (skinned) muscle fiber preparation is widely used to investigate muscle contraction because the intracellular ionic conditions can be precisely controlled. However, plasma membrane removal results in a loss of osmotic regulation, causing abnormal hydration of the myofilament lattice and its proteins. We investigated the structural and functional consequences of varied myofilament lattice spacing and protein hydration on cross-bridge rates of force development and detachment in Drosophila melanogaster indirect flight muscle, using x-ray diffraction to compare the lattice spacing of dissected, osmotically compressed skinned fibers to native muscle fibers in living flies. Osmolytes of different sizes and exclusion properties (Dextran T-500 and T-10) were used to differentially alter lattice spacing and protein hydration. At in vivo lattice spacing, cross-bridge attachment time (t{sub on}) increased with higher osmotic pressures, consistent with a reduced cross-bridge detachment rate as myofilament protein hydration decreased. In contrast, in the swollen lattice, t{sub on} decreased with higher osmotic pressures. These divergent responses were reconciled using a structural model that predicts t{sub on} varies inversely with thick-to-thin filament surface distance, suggesting that cross-bridge rates of force development and detachment are modulated more by myofilament lattice geometry than protein hydration. Generalizing these findings, our results suggest that cross-bridge cycling rates slow as thick-to-thin filament surface distance decreases with sarcomere lengthening, and likewise, cross-bridge cycling rates increase during sarcomere shortening. Together, these structural changes may provide a mechanism for altering cross-bridge performance throughout a contraction-relaxation cycle.

  20. RESULTS AND DISCUSSION -Part I UH60A Rotor in High Speed Forward Flight

    E-Print Network [OSTI]

    , typical of that found on a current generation army helicopter. It has a complex blade form that tends in this chapter is that of a UH-60A rotor in high speed forward flight condition. This case was chosen to test helicopter low speed descent flight. This particular flight condition is dominated by BVI phenomena

  1. Insects owe much of their extraordinary evolutionary success to flight. Compared with their flightless ancestors,

    E-Print Network [OSTI]

    Daniel, Tom

    flapping motion of insects have combined to thwart simple `back-of-the-envelope' explanations of flight simplifying assumptions to build more rigorous models of insect flight. It is this more detailed view have allowed researchers to make rapid progress in advancing our understanding of insect flight

  2. Space System Architecture

    E-Print Network [OSTI]

    McManus, Dr. Hugh

    Final Report of SSPARC: the Space Systems, Policy, and Architecture Research Consortium (Thrust II and III)

  3. 3OURNALOF GEOPHYSICALRESEARCH VOL. 73, NO. 18, SEPTEMBER15, 1968 Commentsonthe Paper by D. G. Rea and B. T. O'Leary,

    E-Print Network [OSTI]

    Fridlind, Ann

    and B. T. O'Leary, ·On the Compositionof the Venus Clouds' JA·ES E. HA·sE· A·D HOWARD CHEYNEY GoddardSpaceFlight Center,Institute [or SpaceStudies,NASA New York, New Yorl· 10025 In a recent paper Rea and O'Leary [1968 causeabsorptionfeaturesat 1.5 and 2.0 · as strong as assumedby Rea and O'Leary. Their conclusionwas basedin part on labora

  4. Can the vertical motions in the eyewall of tropical cyclones support persistent UAV flight?

    E-Print Network [OSTI]

    Poh, Chung-Kiak

    2014-01-01

    Powered flights in the form of manned or unmanned aerial vehicles (UAVs) have been flying into tropical cyclones to obtain vital atmospheric measurements with flight duration typically lasting between 12 and 36 hours. Convective vertical motion properties of tropical cyclones have previously been studied. This work investigates the possibility to achieve persistent flight by harnessing the generally pervasive updrafts in the eyewall of tropical cyclones. A sailplane UAV capable of vertical take-off and landing (VTOL) is proposed and its flight characteristics simulated. Results suggest that the concept of persistent flight within the eyewall is promising and may be extendable to the rainband regions.

  5. Planning, Execution, and Analysis of the Meridian UAS Flight Test Program Including System and Parameter Identification

    E-Print Network [OSTI]

    Tom, Jonathan

    2010-04-27

    systems must be thoroughly tested on the ground before the tested in flight. 3.1.2 Flight Test Limits The Phase I flight test limits for the Meridian are as follows: 1. Manual Flight Time Limit: 30 minutes 2. Maximum Crosswinds: 5 knots 3. Maximum...-of-sight. The maximum crosswinds are limited to 5 knots to ease the difficulty of landing the aircraft. The maximum constant winds are limited to 10 knots of head wind with 5 knots of gust to limit in flight turbulence. Having the wind out of the north...

  6. Social Media: Space Weather #SpaceWeather

    E-Print Network [OSTI]

    causing blackouts in rare cases. To learn about space weather and impacts to the electric grid visit on the Power Grid Space Weather and the Aurora Borealis What are Solar Flares? What are Coronal Mass we do. Satellite communications, GPS applications, and the electric power grid provide the backbone

  7. Parameters’ Covariance in Neutron Time of Flight Analysis – Explicit Formulae

    SciTech Connect (OSTI)

    Odyniec, M.; Blair, J.

    2014-12-01

    We present here a method that estimates the parameters’ variance in a parametric model for neutron time of flight (NToF). The analytical formulae for parameter variances, obtained independently of calculation of parameter values from measured data, express the variances in terms of the choice, settings, and placement of the detector and the oscilloscope. Consequently, the method can serve as a tool in planning a measurement setup.

  8. Two-dimensional Insect Flight on an Air-Water Interface is a Chaotic Oscillator

    E-Print Network [OSTI]

    Mukundarajan, Haripriya; Prakash, Manu

    2014-01-01

    Two-dimensional flapping wing insect flight on an air-water interface provides a successful foraging strategy to explore an ecological niche on the surface of a pond. However, the complex interplay of surface tension, aerodynamic forces, biomechanics and neural control that enables two-dimensional flight is unknown. Here we report the discovery of two-dimensional flight in the waterlily beetle Galerucella nymphaeae, which is the fastest reported propulsion mode for an insect on a fluid interface. Using kinematics derived from high-speed videography coupled with analytical models, we demonstrate that two-dimensional flight is a chaotic interfacial oscillator, thus significantly constraining the possible range of flight parameters. Discovery of this complex dynamics in two-dimensional flight on time scales similar to neural responses indicates the challenge of evolving active flight control on a fluid interface.

  9. Space Science and Applications

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    the first measurements of Earth's space radiation environment and the discovery of gamma-ray bursts. The majority of ISR-1 staff hold PhDs in Space Physics, Nuclear Physics, or...

  10. Senior Space Camp 2015, Andya Space Center, Norway Senior Space Camp 2015

    E-Print Network [OSTI]

    Gerhardy, Philipp

    Senior Space Camp 2015, Andřya Space Center, Norway Senior Space Camp 2015 Arrangřrer: Nasjonalt deltakere Sted: Andřya Space Center (ASC), Andřya, Norway Undervisning: Programmet er delt mellom, Andřya Space Center, Norway FORELESERE / ADMINISTRASJON Tittel Etternavn Fornavn Initialer Organisasjon

  11. Simplest AB-Thermonuclear Space Propulsion and Electric Generator

    E-Print Network [OSTI]

    Alexander Bolonkin

    2007-01-19

    The author applies, develops and researches mini-sized Micro- AB Thermonuclear Reactors for space propulsion and space power systems. These small engines directly convert the high speed charged particles produced in the thermonuclear reactor into vehicle thrust or vehicle electricity with maximum efficiency. The simplest AB-thermonuclear propulsion offered allows spaceships to reach speeds of 20,000 50,000 km/s (1/6 of light speed) for fuel ratio 0.1 and produces a huge amount of useful electric energy. Offered propulsion system permits flight to any planet of our Solar system in short time and to the nearest non-Sun stars by E-being or intellectual robots during a single human life period. Key words: AB-propulsion, thermonuclear propulsion, space propulsion, thermonuclear power system.

  12. In-situ model analysis of STARS missile flight data and comparison to per-flight predictions from test-reconciled models

    SciTech Connect (OSTI)

    James, G.H.; Carne, T.G.; Marek, E.L.

    1994-08-01

    The Natural Excitation Technique (NExT) was used to analyze STARS launch data during first and second stage flight using telemetered acceleration data. A continuous track of modal frequencies and modal damping was acquired for the first and second elastic modes of the system during first stage flight and for the first mode during second stage flight. Generally, the first mode was predicted to be lower than seen in actual flight. The second mode predictions were very close to those seen in flight. Damping values were found to be within the range estimated by ground testing or slightly less. The results from this modal analysis of launch data allowed a final quantification of the inherent bias errors which resulted from the STARS ground-based modal tests as well as pointing out structures which were in need of further test/analysis correlation.

  13. TANK SPACE OPTIONS REPORT

    SciTech Connect (OSTI)

    WILLIS WL; AHRENDT MR

    2009-08-11

    Since this report was originally issued in 2001, several options proposed for increasing double-shell tank (DST) storage space were implemented or are in the process of implementation. Changes to the single-shell tank (SST) waste retrieval schedule, completion of DST space saving options, and the DST space saving options in progress have delayed the projected shortfall of DST storage space from the 2007-2011 to the 2018-2025 timeframe (ORP-11242, River Protection Project System Plan). This report reevaluates options from Rev. 0 and includes evaluations of new options for alleviating projected restrictions on SST waste retrieval beginning in 2018 because of the lack of DST storage space.

  14. NASA ADVISORY COUNCIL COMMERCIAL SPACE COMMITTEE

    E-Print Network [OSTI]

    Waliser, Duane E.

    , operations, and sustaining · Payload and flight science experiment processing, integration and testing · Development, test and demonstration of advanced flight systems and transformational technologies · Developing IRIS ­ Interface Region Imaging Spectrograph TDRS K ­ Tracking and Data Relay System 2013 LDCM

  15. The design and flight performance of the PoGOLite Pathfinder balloon-borne hard X-ray polarimeter

    E-Print Network [OSTI]

    Chauvin, M; Jackson, M; Kamae, T; Kawano, T; Kiss, M; Kole, M; Mikhalev, V; Moretti, E; Olofsson, G; Rydström, S; Takahashi, H; Lind, J; Strömberg, J -E; Welin, O; Iyudin, A; Shifrin, D; Pearce, M

    2015-01-01

    In the 50 years since the advent of X-ray astronomy there have been many scientific advances due to the development of new experimental techniques for detecting and characterising X-rays. Observations of X-ray polarisation have, however, not undergone a similar development. This is a shortcoming since a plethora of open questions related to the nature of X-ray sources could be resolved through measurements of the linear polarisation of emitted X-rays. The PoGOLite Pathfinder is a balloon-borne hard X-ray polarimeter operating in the 25 - 240 keV energy band from a stabilised observation platform. Polarisation is determined using coincident energy deposits in a segmented array of plastic scintillators surrounded by a BGO anticoincidence system and a polyethylene neutron shield. The PoGOLite Pathfinder was launched from the SSC Esrange Space Centre in July 2013. A near-circumpolar flight was achieved with a duration of approximately two weeks. The flight performance of the Pathfinder design is discussed for the...

  16. United States Space Shuttle Firsts

    E-Print Network [OSTI]

    for the open sea test on shuttle retrieval performed at Port Everglades, Florida. 05/01/1979 Enterprise · First. Peterson, S. Musgrave · First flight of the orbiter Challenger. · First Tracking and Data Relay Satellite

  17. Space Systems Finland 1 Deployment in the Space Sector

    E-Print Network [OSTI]

    Southampton, University of

    © Space Systems Finland 1 Deployment in the Space Sector #12;© Space Systems Finland 2 SW Constraints Design Requirements User Requirements SW Requirements #12;© Space Systems Finland 3 The space, but there is no viable alternative · Many requirements are not testable #12;© Space Systems Finland 4 SSF OBJECTIVES

  18. UCL DEPARTMENT OF SPACE & CLIMATE PHYSICS SPACE PLASMA PHYSICS GROUP

    E-Print Network [OSTI]

    Anand, Mahesh

    UCL DEPARTMENT OF SPACE & CLIMATE PHYSICS SPACE PLASMA PHYSICS GROUP ESA Lunar Lander ­ L-DEPP C.J. Owen and D.O. Kataria UCL/MSSL #12;UCL DEPARTMENT OF SPACE & CLIMATE PHYSICS SPACE PLASMA PHYSICS GROUP is LEIA necessary? · Potential UK benefits · Summary #12;UCL DEPARTMENT OF SPACE & CLIMATE PHYSICS SPACE

  19. Matter: Space without Time

    E-Print Network [OSTI]

    Yousef Ghazi-Tabatabai

    2012-11-19

    While Quantum Gravity remains elusive and Quantum Field Theory retains the interpretational difficulties of Quantum Mechanics, we have introduced an alternate approach to the unification of particles, fields, space and time, suggesting that the concept of matter as space without time provides a framework which unifies matter with spacetime and in which we anticipate the development of complete theories (ideally a single unified theory) describing observed 'particles, charges, fields and forces' solely with the geometry of our matter-space-time universe.

  20. Total Space Heat-

    Gasoline and Diesel Fuel Update (EIA)

    Revised: December, 2008 Total Space Heat- ing Cool- ing Venti- lation Water Heat- ing Light- ing Cook- ing Refrig- eration Office Equip- ment Com- puters Other All Buildings...

  1. Total Space Heat-

    Gasoline and Diesel Fuel Update (EIA)

    Released: September, 2008 Total Space Heat- ing Cool- ing Venti- lation Water Heat- ing Light- ing Cook- ing Refrig- eration Office Equip- ment Com- puters Other All Buildings*...

  2. Newtonian Lorentz Metric Spaces

    E-Print Network [OSTI]

    Costea, Serban

    2011-01-01

    This paper studies Newtonian Sobolev-Lorentz spaces. We prove that these spaces are Banach. We also study the global p,q-capacity and the p,q-modulus of families of rectifiable curves. Under some additional assumptions (that is, the space carries a doubling measure and a weak Poincare inequality) and some restrictions on q, we show that the Lipschitz functions are dense in those spaces. Moreover, in the same setting we also show that the p,q-capacity is Choquet provided that q is strictly greater than 1. We provide a counterexample for the density result of Lipschitz functions in the Euclidean setting.

  3. AB Space Engine

    E-Print Network [OSTI]

    Alexander Bolonkin

    2008-03-02

    On 4 January 2007 the author published the article Wireless Transfer of Electricity in Outer Space in http://arxiv.org wherein he offered and researched a new revolutionary method of transferring electric energy in space. In that same article, he offered a new engine which produces a large thrust without throwing away large amounts of reaction mass (unlike the conventional rocket engine). In the current article, the author develops the theory of this kind of impulse engine and computes a sample project which shows the big possibilities opened by this new AB-Space Engine. The AB-Space Engine gets the energy from ground-mounted power; a planet electric station can transfer electricity up to 1000 millions (and more) of kilometers by plasma wires. Author shows that AB-Space Engine can produce thrust of 10 tons (and more). That can accelerate a space ship to some thousands of kilometers/second. AB-Space Engine has a staggering specific impulse owing to the very small mass expended. The AB-Space Engine reacts not by expulsion of its own mass (unlike rocket engine) but against the mass of its planet of origin (located perhaps a thousand of millions of kilometers away) through the magnetic field of its plasma cable. For creating this plasma cable the AB-Space Engine spends only some kg of hydrogen.

  4. Passive solar space heating

    SciTech Connect (OSTI)

    Balcomb, J.D.

    1980-01-01

    An overview of passive solar space heating is presented indicating trends in design, new developments, performance measures, analytical design aids, and monitored building results.

  5. Neutron Tomography and Space

    E-Print Network [OSTI]

    Egbert, Hal; Walker, Ronald; Flocchini, R.

    2007-01-01

    Kevin Shields, “Optimization of neutron tomography for rapidNEUTRON TOMOGRAPHY AND SPACE Hal Egbert, Ronald Walker, R.industrial applications[1]. Neutron Computed Tomography was

  6. Contestation of Space

    E-Print Network [OSTI]

    Alkhalili, Nura

    2012-01-01

    city and a neighboring refugee camp. It seeks to narrate thechange, and the neighboring refugee camp. The public parkoccurring in Ramallah between refugee and non-refugee space.

  7. Multimegawatt space power reactors

    SciTech Connect (OSTI)

    Dearien, J.A.; Whitbeck, J.F.

    1989-01-01

    In response to the need of the Strategic Defense Initiative (SDI) and long range space exploration and extra-terrestrial basing by the National Air and Space Administration (NASA), concepts for nuclear power systems in the multi-megawatt levels are being designed and evaluated. The requirements for these power systems are being driven primarily by the need to minimize weight and maximize safety and reliability. This paper will discuss the present requirements for space based advanced power systems, technological issues associated with the development of these advanced nuclear power systems, and some of the concepts proposed for generating large amounts of power in space. 31 figs.

  8. Space Fiesta - 1 

    E-Print Network [OSTI]

    Unknown

    2011-08-17

    We study the geometric classi?cation of Banach spaces via Lipschitz, uniformly continuous, and coarse mappings. We prove that a Banach space which is uniformly homeomorphic to a linear quotient of lp is itself a linear quotient of lp when p<2...

  9. AB Space Engine

    E-Print Network [OSTI]

    Bolonkin, Alexander

    2008-01-01

    On 4 January 2007 the author published the article Wireless Transfer of Electricity in Outer Space in http://arxiv.org wherein he offered and researched a new revolutionary method of transferring electric energy in space. In that same article, he offered a new engine which produces a large thrust without throwing away large amounts of reaction mass (unlike the conventional rocket engine). In the current article, the author develops the theory of this kind of impulse engine and computes a sample project which shows the big possibilities opened by this new AB-Space Engine. The AB-Space Engine gets the energy from ground-mounted power; a planet electric station can transfer electricity up to 1000 millions (and more) of kilometers by plasma wires. Author shows that AB-Space Engine can produce thrust of 10 tons (and more). That can accelerate a space ship to some thousands of kilometers/second. AB-Space Engine has a staggering specific impulse owing to the very small mass expended. The AB-Space Engine reacts not b...

  10. Moduli Spaces and Grassmannian

    E-Print Network [OSTI]

    Jia-Ming Liou; Albert Schwarz

    2012-04-12

    We calculate the homomorphism of the cohomology induced by the Krichever map of moduli spaces of curves into infinite-dimensional Grassmannian. This calculation can be used to compute the homology classes of cycles on moduli spaces of curves that are defined in terms of Weierstrass points.

  11. SPACE TECHNOLOGY Actual Estimate

    E-Print Network [OSTI]

    technology readiness of new missions, mitigate their technological risks, improve the quality of cost estimates, and thereby contribute to better overall mission cost management..." Space Technology investmentsSPACE TECHNOLOGY TECH-1 Actual Estimate Budget Authority (in $ millions) FY 2011 FY 2012 FY 2013 FY

  12. Atoms for space

    SciTech Connect (OSTI)

    Buden, D.

    1990-10-01

    Nuclear technology offers many advantages in an expanded solar system space exploration program. These cover a range of possible applications such as power for spacecraft, lunar and planetary surfaces, and electric propulsion; rocket propulsion for lunar and Mars vehicles; space radiation protection; water and sewage treatment; space mining; process heat; medical isotopes; and self-luminous systems. In addition, space offers opportunities to perform scientific research and develop systems that can solve problems here on Earth. These might include fusion and antimatter research, using the Moon as a source of helium-3 fusion fuel, and manufacturing perfect fusion targets. In addition, nuclear technologies can be used to reduce risk and costs of the Space Exploration Initiative. 1 fig.

  13. Linear electronic field time-of-flight ion mass spectrometers

    DOE Patents [OSTI]

    Funsten, Herbert O. (Los Alamos, NM)

    2010-08-24

    Time-of-flight mass spectrometer comprising a first drift region and a second drift region enclosed within an evacuation chamber; a means of introducing an analyte of interest into the first drift region; a pulsed ionization source which produces molecular ions from said analyte of interest; a first foil positioned between the first drift region and the second drift region, which dissociates said molecular ions into constituent atomic ions and emits secondary electrons; an electrode which produces secondary electrons upon contact with a constituent atomic ion in second drift region; a stop detector comprising a first ion detection region and a second ion detection region; and a timing means connected to the pulsed ionization source, to the first ion detection region, and to the second ion detection region.

  14. Initial Results from the ANITA 2006-2007 Balloon Flight

    SciTech Connect (OSTI)

    Gorham, P.W.; Allison, P.; Barwick, S.W.; Beatty, J.J.; Besson, D.Z.; Binns, W.R.; Chen, C.; Chen, P.; Clem, J.M.; Connolly, A.; Dowkontt, P.F.; DuVernois, M.A.; Field, R.C.; Goldstein, D.; Goodhue, A.; Hast, C.; Hebert, C.L.; Hoover, S.; Israel, M.H.; Kowalski, J.; Learned, J.G.; /Hawaii U. /Caltech, JPL /Hawaii U. /Minnesota U. /Hawaii U. /Ohio State U. /Hawaii U. /Hawaii U. /UC, Irvine /Taiwan, Natl. Taiwan U. /Caltech, JPL /SLAC /University Coll. London /Ohio State U. /SLAC /Hawaii U. /Hawaii U. /Hawaii U. /UCLA /Delaware U. /Hawaii U. /SLAC /Taiwan, Natl. Taiwan U. /UC, Irvine

    2011-11-16

    We report initial results of the Antarctic Impulsive Transient Antenna (ANITA) 2006-2007 Long Duration Balloon flight, which searched for evidence of the flux of cosmogenic neutrinos. ANITA flew for 35 days looking for radio impulses that might be due to the Askaryan effect in neutrino-induced electromagnetic showers within the Antarctic ice sheets. In our initial high-threshold robust analysis, no neutrino candidates are seen, with no physics background. In a non-signal horizontal-polarization channel, we do detect 6 events consistent with radio impulses from extensive air showers, which helps to validate the effectiveness of our method. Upper limits derived from our analysis now begin to eliminate the highest cosmogenic neutrino models.

  15. Inverse time-of-flight spectrometer for beam plasma research

    SciTech Connect (OSTI)

    Yushkov, Yu. G., E-mail: yuyushkov@gmail.com; Zolotukhin, D. B.; Tyunkov, A. V. [Tomsk State University of Control Systems and Radioelectronics, 40 Lenin Ave., Tomsk 634050 (Russian Federation); Oks, E. M. [Tomsk State University of Control Systems and Radioelectronics, 40 Lenin Ave., Tomsk 634050 (Russian Federation); Institute of High Current Electronics SB RAS, 2/3, Akademichesky Ave., Tomsk 634055 (Russian Federation); Savkin, K. P. [Institute of High Current Electronics SB RAS, 2/3, Akademichesky Ave., Tomsk 634055 (Russian Federation)

    2014-08-15

    The paper describes the design and principle of operation of an inverse time-of-flight spectrometer for research in the plasma produced by an electron beam in the forevacuum pressure range (5–20 Pa). In the spectrometer, the deflecting plates as well as the drift tube and the primary ion beam measuring system are at high potential with respect to ground. This provides the possibility to measure the mass-charge constitution of the plasma created by a continuous electron beam with a current of up to 300 mA and electron energy of up to 20 keV at forevacuum pressures in the chamber placed at ground potential. Research results on the mass-charge state of the beam plasma are presented and analyzed.

  16. Highly charged ion based time of flight emission microscope

    DOE Patents [OSTI]

    Barnes, Alan V. (Livermore, CA); Schenkel, Thomas (San Francisco, CA); Hamza, Alex V. (Livermore, CA); Schneider, Dieter H. (Livermore, CA); Doyle, Barney (Albuquerque, NM)

    2001-01-01

    A highly charged ion based time-of-flight emission microscope has been designed, which improves the surface sensitivity of static SIMS measurements because of the higher ionization probability of highly charged ions. Slow, highly charged ions are produced in an electron beam ion trap and are directed to the sample surface. The sputtered secondary ions and electrons pass through a specially designed objective lens to a microchannel plate detector. This new instrument permits high surface sensitivity (10.sup.10 atoms/cm.sup.2), high spatial resolution (100 nm), and chemical structural information due to the high molecular ion yields. The high secondary ion yield permits coincidence counting, which can be used to enhance determination of chemical and topological structure and to correlate specific molecular species.

  17. Thermal soaring flight of birds and unmanned aerial vehicles

    E-Print Network [OSTI]

    Ákos, Zsuzsa; Leven, Severin; Vicsek, Tamás; 10.1088/1748-3182/5/4/045003

    2010-01-01

    Thermal soaring saves much energy, but flying large distances in this form represents a great challenge for birds, people and Unmanned Aerial Vehicles (UAVs). The solution is to make use of so-called thermals, which are localized, warmer regions in the atmosphere moving upwards with a speed exceeding the descent rate of birds and planes. Saving energy by exploiting the environment more efficiently is an important possibility for autonomous UAVs as well. Successful control strategies have been developed recently for UAVs in simulations and in real applications. This paper first presents an overview of our knowledge of the soaring flight and strategy of birds, followed by a discussion of control strategies that have been developed for soaring UAVs both in simulations and applications on real platforms. To improve the accuracy of simulation of thermal exploitation strategies we propose a method to take into account the effect of turbulence. Finally we propose a new GPS independent control strategy for exploiting...

  18. Flight Measurements of the Aero-Optical Environment Around a Flat-Windowed Turret

    E-Print Network [OSTI]

    Gordeyev, Stanislav

    Flight Measurements of the Aero-Optical Environment Around a Flat-Windowed Turret Chris Porter.2514/1.J052067 This paper discusses the aero-optical environment for a flat-window hemisphere-on-cylinder turret over a wide range of viewing angles during flight tests in the Airborne Aero-Optics Laboratory

  19. RESULTS AND DISCUSSION Part II AH-1G ROTOR IN LOW SPEED DESCENT FLIGHT

    E-Print Network [OSTI]

    ;5.1 Details of the Flight Test A flight test of the AH-1G helicopter was performed at NASA Ames Research and Acoustics Test (TAAT) was conducted on an AH-1G Cobra. It used highly instrumented rotor blades collected from a few pressure ports on the blade. Several calculations for this helicopter have been

  20. FLIGHT SIMULATION FOR THE DEVELOPMENT OF AN EXPERIMENTAL UAV Eric N. Johnson* and Sumit Mishra

    E-Print Network [OSTI]

    Johnson, Eric N.

    FLIGHT SIMULATION FOR THE DEVELOPMENT OF AN EXPERIMENTAL UAV Eric N. Johnson* and Sumit Mishra Uninhabited Aerial Vehicle (UAV) system. These types of UAV systems are characterized by the need for the need by complementing research results with flight-test validated simulation results for the same experimental UAV

  1. Sex-specific development of avian flight performance under experimentally altered

    E-Print Network [OSTI]

    starling, flight ability, predation risk, sexual size dimorphism. [Behav Ecol 18:967­973 (2007)] In birds for variation in flight perfor- mance in juvenile European starlings (Sturnus vulgaris), a sexually size-dimorphic conditions in sexually size-dimorphic species. Key words: development, escape perfor- mance, european

  2. Formal Modeling and Verification of Operational Flight Program in a Small-Scale Unmanned Helicopter

    E-Print Network [OSTI]

    Formal Modeling and Verification of Operational Flight Program in a Small-Scale Unmanned Helicopter helicopter and its onboard embedded computing system for flight control and real-time transmission and application services for an unmanned helicopter. It will be used for responding to disasters such as forest

  3. AFRL TRB & SRB SUPPLEMENT 3 Aug 07 Review of DRE technology and flight

    E-Print Network [OSTI]

    1 AFRL ­ TRB & SRB SUPPLEMENT 3 Aug 07 Review of DRE technology and flight experiments at Rec = 7;2 AFRL ­ TRB & SRB SUPPLEMENT 3 Aug 07 OUTLINE · Highlights from ASU wind-tunnel exp · Texas A&M flight experiments (AFRL/AFOSR) · Ongoing work #12;3 AFRL ­ TRB & SRB SUPPLEMENT 3 Aug 07 Highlights from ASU wind

  4. Design of an Optimal Flight Control System with Integral Augmented Compensator for a Nonlinear UAV Helicopter

    E-Print Network [OSTI]

    Li, Yangmin

    Design of an Optimal Flight Control System with Integral Augmented Compensator for a Nonlinear UAV presents the development of an optimal flight control system for a small-scale Unmanned Aerial Vehicle (UAV and the controller design. In this work, the comprehensive nonlinear model of the helicopter system is derived from

  5. Using Time-of-Flight Measurements for Privacy-Preserving Tracking in a Smart Room

    E-Print Network [OSTI]

    Radke, Rich

    for human assistance, or even detect anomalies in occupant behavior (e.g., alerting staff if an occupant-of-flight images are severely downsampled to preserve the privacy of the occupants and simulate future applications-of-flight, smart room, pose recognition, visual tracking, privacy preservation, occupancy detection I. INTRODUCTION

  6. LSPE Qualification and Flight Acceptance T /V Test Su.m..mary and Thermal Design

    E-Print Network [OSTI]

    Rathbun, Julie A.

    LSPE Qualification and Flight Acceptance T /V Test Su.m..mary and Thermal Design Final Report NO. ATM 1110 This ATM Summarizes the analytical and test results of the Lunar Seismic Profiling Experiment summarizes the Qualification and Flight Acceptance thermal vacuum testing programs and the third section

  7. Weakly Ionized Plasmas in Hypersonics: Fundamental Kinetics and Flight Applications

    SciTech Connect (OSTI)

    Macheret, Sergey

    2005-05-16

    The paper reviews some of the recent studies of applications of weakly ionized plasmas to supersonic/hypersonic flight. Plasmas can be used simply as means of delivering energy (heating) to the flow, and also for electromagnetic flow control and magnetohydrodynamic (MHD) power generation. Plasma and MHD control can be especially effective in transient off-design flight regimes. In cold air flow, nonequilibrium plasmas must be created, and the ionization power budget determines design, performance envelope, and the very practicality of plasma/MHD devices. The minimum power budget is provided by electron beams and repetitive high-voltage nanosecond pulses, and the paper describes theoretical and computational modeling of plasmas created by the beams and repetitive pulses. The models include coupled equations for non-local and unsteady electron energy distribution function (modeled in forward-back approximation), plasma kinetics, and electric field. Recent experimental studies at Princeton University have successfully demonstrated stable diffuse plasmas sustained by repetitive nanosecond pulses in supersonic air flow, and for the first time have demonstrated the existence of MHD effects in such plasmas. Cold-air hypersonic MHD devices are shown to permit optimization of scramjet inlets at Mach numbers higher than the design value, while operating in self-powered regime. Plasma energy addition upstream of the inlet throat can increase the thrust by capturing more air (Virtual Cowl), or it can reduce the flow Mach number and thus eliminate the need for an isolator duct. In the latter two cases, the power that needs to be supplied to the plasma would be generated by an MHD generator downstream of the combustor, thus forming the 'reverse energy bypass' scheme. MHD power generation on board reentry vehicles is also discussed.

  8. UCL DEPARTMENT OF SPACE & CLIMATE PHYSICS SPACE PLASMA PHYSICS GROUP

    E-Print Network [OSTI]

    UCL DEPARTMENT OF SPACE & CLIMATE PHYSICS SPACE PLASMA PHYSICS GROUP 18th September 2012 STFC Summer School An Introduction to the Structure of the Magnetosphere Prof. Chris Owen Mullard Space 2012 #12;UCL DEPARTMENT OF SPACE & CLIMATE PHYSICS SPACE PLASMA PHYSICS GROUP 18th September 2012 STFC

  9. Quotients of Metric Spaces

    E-Print Network [OSTI]

    Herman, Robert A.

    1968-01-01

    . PRELIMINARIES 1 CHAPTER II . SFACBS IN WHICH SEQUENCES SUFFICE 6 CHAPTER III . QUOTIENTS OF SEPARABLE METRIC SPACES Ik CHAPTER IV. GENERAL QUOTIENT SPACES 25 CHAPTER V. CLOSED QUOTIENT MAPS 35 CHAPTER VI. OPEN QUOTIENT MAPS 50 CHAPTER VII. OPEN AND CLOSED... QUOTIENT MAPS 55 CHAPTER VIII. ANOTHER RESULT 6l BIBLIOGRAPHY 65 CHAPTER I. PRELIMINARIES We begin by stating some basic definitions and theorems. Definition 1 . 1 ; Let f be a function from a topological space X onto a set Y. Then the quotient...

  10. A flight test system for the determination of the stability and control derivatives of a general aviation aircraft 

    E-Print Network [OSTI]

    Oehl, David Christopher

    1995-01-01

    This volume documents the research effort which provided a flight test system and flight data to determine the stability and control derivatives for the Rockwell Commander N700AE aircraft. The presented research was conducted from June 1994 to May...

  11. Invited Review Article: Advanced light microscopy for biological space research

    SciTech Connect (OSTI)

    De Vos, Winnok H.; Beghuin, Didier; Schwarz, Christian J.; Jones, David B.; Loon, Jack J. W. A. van

    2014-10-15

    As commercial space flights have become feasible and long-term extraterrestrial missions are planned, it is imperative that the impact of space travel and the space environment on human physiology be thoroughly characterized. Scrutinizing the effects of potentially detrimental factors such as ionizing radiation and microgravity at the cellular and tissue level demands adequate visualization technology. Advanced light microscopy (ALM) is the leading tool for non-destructive structural and functional investigation of static as well as dynamic biological systems. In recent years, technological developments and advances in photochemistry and genetic engineering have boosted all aspects of resolution, readout and throughput, rendering ALM ideally suited for biological space research. While various microscopy-based studies have addressed cellular response to space-related environmental stressors, biological endpoints have typically been determined only after the mission, leaving an experimental gap that is prone to bias results. An on-board, real-time microscopical monitoring device can bridge this gap. Breadboards and even fully operational microscope setups have been conceived, but they need to be rendered more compact and versatile. Most importantly, they must allow addressing the impact of gravity, or the lack thereof, on physiologically relevant biological systems in space and in ground-based simulations. In order to delineate the essential functionalities for such a system, we have reviewed the pending questions in space science, the relevant biological model systems, and the state-of-the art in ALM. Based on a rigorous trade-off, in which we recognize the relevance of multi-cellular systems and the cellular microenvironment, we propose a compact, but flexible concept for space-related cell biological research that is based on light sheet microscopy.

  12. Total Space Heat-

    Gasoline and Diesel Fuel Update (EIA)

    Survey: Energy End-Use Consumption Tables Total Space Heat- ing Cool- ing Venti- lation Water Heat- ing Light- ing Cook- ing Refrig- eration Office Equip- ment Com- puters Other...

  13. Notes on sexuality & space

    E-Print Network [OSTI]

    Jacobson, Samuel Ray

    2013-01-01

    Very little has been written on sexuality in architectural scholarship. Sexuality & Space (Princeton Architectural Press, 1992) contains the proceedings of an eponymous 1990 conference at Princeton University, and was both ...

  14. Saving Space in China

    E-Print Network [OSTI]

    Hacker, Randi

    2013-09-09

    Broadcast Transcript: The Chinese are geniuses at utilizing every inch of space. In a country that is historically overcrowded, this skill is important for survival. Chinese vegetable gardens are miracles of permaculture layout: small plants nestle...

  15. Commutators on Banach Spaces 

    E-Print Network [OSTI]

    Dosev, Detelin

    2010-10-12

    . In particular, we will focus our attention to the spaces $\\lambda I and $\\linf$. The main results are that the commutators on $\\ell_1$ are the operators not of the form $\\lambda I + K$ with $\\lambda\

  16. Electronics for a Picosecond Time-of-flight Measurement

    SciTech Connect (OSTI)

    Brandt, Andrew Gerhart; Rijssenbeek, Michael

    2014-11-03

    TITLE: Electronics for a Picosecond Time-of-flight Measurement ABSTRACT: Time-of-flight (TOF) detectors have historically been used as part of the particle identification capability of multi-purpose particle physics detectors. An accurate time measurement, combined with a momentum measurement based on the curvature of the track in a magnetic field, is often sufficient to determine the particle's mass, and thus its identity. Such detectors typically have measured the particle flight time extremely precisely, with an uncertainty of one hundred trillionths of a second (also referred to as 100 picoseconds). To put this in perspective it would be like counting all the people on the Earth and getting it right within 1 person! Another use of TOFs is to measure the vertex of the event, which is the location along the beam line where the incoming particles (typically protons) collide. This vertex positon is a well measured quantity for events where the protons collide “head on” as the outgoing particles produced when you blast the proton apart can be used to trace back to a vertex point from which they originated. More frequently the protons just strike a glancing blow and remain intact—in this case they are nearly parallel to the beam and you cannot tell their vertex without this ability to precisely measure the time of flight of the protons. Occasionally both happen in the same event, that is, a central system and two protons are produced. But are they from the same collision, or just a boring background where more than one collision in the same bunch crossing conspire to fake the signal of interest? That’s where the timing of the protons comes into play. The main idea is to measure the time it takes for the two protons to reach TOF detectors positioned equidistant from the center of the main detector. If the vertex is displaced to one side than that detector will measure a shorter time while the other side detector will measure a correspondingly longer time. Taking into account the speed of the particles, which is very close to the speed of light, an accuracy of 100 ps gives a vertex measurement of a few cm or a little more than an inch. At the Large Hadron Collider, where there are up to a hundred billion protons per bunch, and the collision region is compressed to a few inches, that is just not good enough. A higher level of precision is needed to determine whether the vertex of the protons and that of the central system are the same. A factor 10 improvement in the timing measurement to the 10 trillionths of a second level, for example would give the requisite 10 times improvement in the vertex measurement. An accurate measurement of the flight time depends on three key elements: the radiator that produces light when the proton passes through it, the photo-sensor that converts the light to an electrical signal, and the electronics that convert this electrical signal into a time measurement with a compact recordable format. With recent improvements in detector design featuring a series of quartz radiators connected to a micro-channel plate photomultiplier tube, this superior measurement capability is within reach if the readout electronics are sufficiently performant. As a result of the funding of this proposal, we have achieved our primary goals. 1) We have developed from scratch or improved upon existing designs of the full chain of electronics that can maintain the performance of a TOF detector from the output of the photo-sensor to the recording of a compressed data packet containing the timing information. We have accomplished this with a cost effective modular approach such that some or all of the components in the chain could easily be adapted for use in diverse particle physics experiments or in other areas where precise timing is required, such as medical and homeland security devices.

  17. MODELING THE EFFECTS OF HUD VISUAL PROPERTIES, PILOT EXPERIENCE AND FLIGHT SCENARIO ON A MULTI-DIMENSIONAL MEASURE OF CLUTTER

    E-Print Network [OSTI]

    Kaber, David B.

    MODELING THE EFFECTS OF HUD VISUAL PROPERTIES, PILOT EXPERIENCE AND FLIGHT SCENARIO ON A MULTI experience; (b) HUD configuration; (c) flight segment; and (d) workload on perceptions of display clutter and cognitive load, and flight task performance. 3. Model HUD clutter scores in terms of display visual

  18. Alpha Magnetic Spectrometer (AMS02) experiment on the International Space Station (ISS)

    E-Print Network [OSTI]

    Behcet Alpat

    2003-08-27

    The Alpha Magnetic Spectrometer experiment is realized in two phases. A precursor flight (STS-91) with a reduced experimental configuration (AMS01) has successfully flown on space shuttle Discovery in June 1998. The final version (AMS02) will be installed on the International Space Station (ISS) as an independent module in early 2006 for an operational period of three years. The main scientific objectives of AMS02 include the searches for the antimatter and dark matter in cosmic rays. In this work we will discuss the experimental details as well as the improved physics capabilities of AMS02 on ISS.

  19. National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Rathbun, Julie A.

    ,,/ NASA National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston by the National Aeronautics and Space Administration ii Hosted by the National Academy of Sclences for library, abstract service, educational, or research purposes; however, republication of any paper

  20. China's Space Robotic Arms Programs

    E-Print Network [OSTI]

    POLLPETER, Kevin

    2013-01-01

    2013 China’s Space Robotic Arm Programs Kevin POLLPETERdebris observation and space robotic arm technologies. Thelikely equipped with a robotic arm, grappling the target

  1. Debris and Future Space Activities

    E-Print Network [OSTI]

    California at Santa Cruz, University of

    Debris and Future Space Activities Prof. Joel R. Primack Physics Department University would be endangered. Every person who cares about the human future in space should also realize

  2. Flight-systems-safety program. Progress report, May 1982

    SciTech Connect (OSTI)

    Bronisz, S.E. (comp.)

    1982-10-01

    This technical monthly report covers studies related to the use of /sup 238/PuO/sub 2/ in radioisotope power systems carried out for the Office of Space Nuclear Projects of the US Department of Energy by Los Alamos National Laboratory. Most of the studies discussed here are ongoing. Results and conclusions described may change as the work continues.

  3. CoordinatorBenjamin C. Young, Capt, Recruiting Flight Commander

    E-Print Network [OSTI]

    Capogna, Luca

    at the University of Arkansas. OurPurpose Fall Semester Freshman AERO 1011 The Foundations of the US Air Force I AERO 1011L Lab and Physical Training Sophomore AERO 2011 The Evolution of Air and Space Power I AERO 2011L Lab and Physical Training Spring Semester Freshman AERO 1021 The Foundations of the US Air Force

  4. Alex Riordan Brian Pruitt-Goddard

    E-Print Network [OSTI]

    Huang, Chun-Hsi

    with the following selections: New File, Save, Save As, Open, and Recent as well as the following via the MORE button is pressed, the user is prompted with whether they would like to save it before opening a new file. If they would, they are redirected to the Save As screen. Once the previous file has been saved (if applicable

  5. Goddard, Kansas: Energy Resources | Open Energy Information

    Open Energy Info (EERE)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on QA:QAsource History View New PagesSustainableGlynn County, Georgia: Energy Resources Jump to:

  6. Proceedings of the 12th Space Photovoltaic Research and Technology Conference (SPRAT 12)

    SciTech Connect (OSTI)

    1993-05-01

    The Twelfth Space Photovoltaic Research and Technology conference was held at the NASA Lewis Research Center from 20 to 22 Oct. 1992. The papers and workshops presented in this volume report substantial progress in a variety of areas in space photovoltaics. Topics covered include: high efficiency GaAs and InP solar cells, GaAs/Ge cells as commercial items, flexible amorphous and thin film solar cells (in the early stages of pilot production), high efficiency multiple bandgap cells, laser power converters, solar cell and array technology, heteroepitaxial cells, betavoltaic energy conversion, and space radiation effects in InP cells. Space flight data on a variety of cells were also presented. Separate abstracts have been prepared for articles from this report.

  7. Validation of an in-flight flow visualization scheme to quantitatively measure vortical flow phenomena 

    E-Print Network [OSTI]

    Dorsett, Kenneth Merle

    1993-01-01

    A flow visualization measurement scheme was validated in flight. Strake vortex trajectories and axial core velocities were determined using pulsed smoke and high speed video. A gothic strake, operated at an angle of attack of 220 and a Reynolds...

  8. Quantifying Peptides in Isotopically Labeled Protease Digests by Ion Mobility/Time-of-Flight

    E-Print Network [OSTI]

    Clemmer, David E.

    Quantifying Peptides in Isotopically Labeled Protease Digests by Ion Mobility/Time-of-Flight Mass-terminus can be accomplished by digesting proteins in 18O-labeled water,11-20 resulting in incorpora- tion

  9. Measurement of the Translational Energy of Ions with a Time?of?Flight Mass Spectrometer

    E-Print Network [OSTI]

    Franklin, J. L.; Hierl, Peter M.; Whan, David A.

    1967-01-01

    A mathematical analysis of peak shapes in a Bendix time?of?flight mass spectrometer shows that ions formed with excess translational energy exhibit considerable peak broadening. A method is developed by which this translational ...

  10. Quantifying the Impact of Flight Predictability on Strategic and Operational Airline Decisions

    E-Print Network [OSTI]

    Hao, Lu

    2015-01-01

    55 Table 4.1 Estimation Results for Fuel Upliftfor an flight, termed fuel uplift, is a much more delicatewith the effect of fuel uplift on fuel burn, suggests a

  11. Fractal morphology, imaging and mass spectrometry of single aerosol particles in flight (CXIDB ID 16)

    DOE Data Explorer [Office of Scientific and Technical Information (OSTI)]

    Loh, N. Duane

    2012-06-20

    This deposition includes the aerosol diffraction images used for phasing, fractal morphology, and time-of-flight mass spectrometry. Files in this deposition are ordered in subdirectories that reflect the specifics.

  12. Wireless Stimulation of Antennal Muscles in Freely Flying Hawkmoths Leads to Flight Path Changes

    E-Print Network [OSTI]

    Hinterwirth, Armin J.

    Insect antennae are sensory organs involved in a variety of behaviors, sensing many different stimulus modalities. As mechanosensors, they are crucial for flight control in the hawkmoth Manduca sexta. One of their roles ...

  13. Wind Tunnel and Flight Testing of Active Flow Control on a UAV 

    E-Print Network [OSTI]

    Babbar, Yogesh

    2011-08-08

    Active flow control has been extensively explored in wind tunnel studies but successful in-flight implementation of an active flow control technology still remains a challenge. This thesis presents implementation of active flow control technology...

  14. Intelligent executive guidance agent for general aviation aircraft under free flight 

    E-Print Network [OSTI]

    Rong, Jie

    2002-01-01

    situation within this environment occurs when multiple traffic and weather conflicts arise simultaneously. A solution that forms the basis for this thesis is an agent based hierarchical system that attempts to provide optimal and conflict free flight path...

  15. FIBER-OPTIC PRESSURE SENSOR FOR TIME-OF-FLIGHT MEASUREMENTS IN A SHOCK WAVE

    E-Print Network [OSTI]

    Texas at Arlington, University of

    temperatures as encountered in combustors. To ensure high-temperature survivability, such sensors may be bonded the pressure pulse and the time-of-flight (TOF) of a propagating detonation wave for implementation shock tubes

  16. Fractal morphology, imaging and mass spectrometry of single aerosol particles in flight (CXIDB ID 16)

    DOE Data Explorer [Office of Scientific and Technical Information (OSTI)]

    Loh, N. Duane

    This deposition includes the aerosol diffraction images used for phasing, fractal morphology, and time-of-flight mass spectrometry. Files in this deposition are ordered in subdirectories that reflect the specifics.

  17. Physically-based aerodynamic flight of birds: an interactive approach to behavioral flocking 

    E-Print Network [OSTI]

    Ringham, Michael Lynn

    1996-01-01

    This thesis describes a method for simulating the flight of birds in a flock with the use of physically-based aerodynamics. The resulting flocking behavior dramatically improves on results previously obtained in computer graphics and animation...

  18. Airline alliance revenue management : improving joint revenues through partner sharing of flight leg opportunity costs

    E-Print Network [OSTI]

    Michel, Alyona

    2012-01-01

    Airlines participating in alliances offer code share itineraries (with flight segments operated by different partners) to expand the range of origin-destination combinations offered to passengers, thus increasing market ...

  19. Guidance and control using model predictive control for low altitude real-time terrain following flight

    E-Print Network [OSTI]

    Lapp, Tiffany Rae, 1979-

    2004-01-01

    This thesis presents the design and implementation of a model predictive control based trajectory optimization method for Nap-of-the-Earth (NOE) flight. A NOE trajectory reference is generated over a subspace of the terrain. ...

  20. Stability derivative extraction from flight test data for a general aviation aircraft 

    E-Print Network [OSTI]

    Randall, Brian Edward

    1996-01-01

    inputs compared well with the flight test data. However, the modeled response to an aileron input did not emulate the aircraft response since the models produced adverse rather than proverse yaw. In general, the stability derivatives and flying qualities...

  1. Control, estimation, and planning algorithms for aggressive flight using onboard sensing

    E-Print Network [OSTI]

    Bry, Adam Parker

    2012-01-01

    This thesis is motivated by the problem of fixed-wing flight through obstacles using only on-board sensing. To that end, we propose novel algorithms in trajectory generation for fixed-wing vehicles, state estimation in ...

  2. Poster Abstract: Practical Limits of WiFi Time-of-Flight Echo Techniques

    E-Print Network [OSTI]

    Lenders, Vincent

    Giustiniano Institute IMDEA Networks Madrid, Spain domenico.giustiniano@imdea.org Vincent Lenders Armasuisse Thun, Switzerland vincent.lenders@armasuisse.ch Abstract--Time-of-flight echo techniques have been

  3. Strain and particle size of palladium powders by time-of-flight neutron diffraction

    SciTech Connect (OSTI)

    Lawson, A.C.; Conant, J.W.; Talcott, C.L.; David, M.A.; Vaninetti, J.; Goldstone, J.A.; Williams, A.; Von Dreele, R.B.; Roof, R.B.; Hitterman, R.L.; Richardson, J.W. Jr.; Faber, J. Jr.

    1989-01-01

    We have determined the strain and particle size for several samples of palladium powder by time-of-flight neutron powder diffraction on two different diffractometers and by x-ray powder diffraction. The results are compared and found to be in fair agreement. The time-of-flight method gives good enough precision to reveal deficiencies in the simple models used for strain and particle size line broadening. 6 refs., 4 figs., 2 tabs.

  4. Flight to Quality? An Investigation of Changing Price Spreads in Commercial Real Estate Markets

    E-Print Network [OSTI]

    Fuerst, Franz; McAllister, Patrick; Sivitanides, Petros

    2015-01-01

    were positively correlated. However, supporting the flight- to-quality hypothesis they also found evidence that, in some “extreme” situations, this relationship turned negative. Hartmann, Straetmans and de Vries (2004), found that flight of capital... . (1989) The Motivation for Institutional Real Estate Sales and Implications for Asset Class Returns, AREUEA Journal, 17, 1, 70- 82 Hartmann, P. S. Straetmans and C. G. De Vries. 2004. Asset Market Linkages in Crisis Periods. The Review of Economics...

  5. National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Xu, Kun

    National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681 Aeronautics a

  6. space holder Fisheries Economics

    E-Print Network [OSTI]

    #12;#12;space holder Fisheries Economics of the United States, 2011 Economics and Social Analysis Citation: National Marine Fisheries Service. 2012. Fisheries Economics of the United States, 2011. U/publication/index.html. A copy of this report may be obtained from: Economics and Social Analysis Division

  7. The Flight Spectral Response of the ACIS Instrument

    E-Print Network [OSTI]

    Paul P. Plucinsky; Norbert S. Schulz; Herman L. Marshall; Catherine E. Grant; George Chartas; Divas Sanwal; Marcus A. Teter; Alexey A. Vikhlinin; Richard J. Edgar; Michael W. Wise; Glenn E. Allen; Shanil N. Virani; Joseph M. DePasquale; Michael T. Raley

    2002-09-24

    We discuss the flight calibration of the spectral response of the Advanced CCD Imaging Spectrometer (ACIS) on-board the Chandra X-ray Observatory (CXO). The spectral resolution and sensitivity of the ACIS instrument have both been evolving over the course of the mission. The spectral resolution of the frontside-illuminated (FI) CCDs changed dramatically in the first month of the mission due to radiation damage. Since that time, the spectral resolution of the FI CCDs and the backside-illuminated (BI) CCDs have evolved gradually with time. We demonstrate the efficacy of charge-transfer inefficiency (CTI) correction algorithms which recover some of the lost performance. The detection efficiency of the ACIS instrument has been declining throughout the mission, presumably due to a layer of contamination building up on the filter and/or CCDs. We present a characterization of the energy dependence of the excess absorption and demonstrate software which models the time dependence of the absorption from energies of 0.4 keV and up. The spectral redistribution function and the detection efficiency are well-characterized at energies from 1.5 to 8.0 keV. The calibration at energies below 1.5 keV is challenging because of the lack of strong lines in the calibration source and also because of the inherent non-linear dependence with energy of the CTI and the absorption by the contamination layer. We have been using data from celestial sources with relatively simple spectra to determine the quality of the calibration below 1.5 keV. The analysis of these observations demonstrate that the CTI correction recovers a significant fraction of the spectral resolution of the FI CCDs and the models of the time-dependent absorption result in consistent measurements of the flux at low energies for data from a BI (S3) CCD.

  8. Orbit Spaces in Superconductivity

    E-Print Network [OSTI]

    Vittorino Talamini

    2006-07-30

    In the framework of Landau theory of phase transitions one is interested to describe all the possible low symmetry ``superconducting'' phases allowed for a given superconductor crystal and to determine the conditions under which this crystal undergoes a phase transition. These problems are best described and analyzed in the orbit space of the high symmetry group of the ``normal, non-superconducting'' phase of the crystal. In this article it is worked out a simple example concerning superconductivity, that shows the P-matrix method to determine the equations and inequalities defining the orbit space and its stratification. This approach is of general validity and can be used in all physical problems that make use of invariant functions, as long as the symmetry group is compact.

  9. Nuclear electric propulsion for future NASA space science missions

    SciTech Connect (OSTI)

    Yen, Chen-wan L.

    1993-07-20

    This study has been made to assess the needs, potential benefits and the applicability of early (circa year 2000) Nuclear Electric Propulsion (NEP) technology in conducting NASA science missions. The study goals are: to obtain the performance characteristics of near term NEP technologies; to measure the performance potential of NEP for important OSSA missions; to compare NEP performance with that of conventional chemical propulsion; to identify key NEP system requirements; to clarify and depict the degree of importance NEP might have in advancing NASA space science goals; and to disseminate the results in a format useful to both NEP users and technology developers. This is a mission performance study and precludes investigations of multitudes of new mission operation and systems design issues attendant in a NEP flight.

  10. Composition pulse time-of-flight mass flow sensor

    DOE Patents [OSTI]

    Harnett, Cindy K. (Livermore, CA); Crocker, Robert W. (Fremont, CA); Mosier, Bruce P. (San Francisco, CA); Caton, Pamela F. (Berkeley, CA); Stamps, James F. (Livermore, CA)

    2007-06-05

    A device for measuring fluid flow rates over a wide range of flow rates (<1 nL/min to >10 .mu.L/min) and at pressures at least as great as 2,000 psi. The invention is particularly adapted for use in microfluidic systems. The device operates by producing compositional variations in the fluid, or pulses, that are subsequently detected downstream from the point of creation to derive a flow rate. Each pulse, comprising a small fluid volume, whose composition is different from the mean composition of the fluid, can be created by electrochemical means, such as by electrolysis of a solvent, electrolysis of a dissolved species, or electrodialysis of a dissolved ionic species. Measurements of the conductivity of the fluid can be used to detect the arrival time of the pulses, from which the fluid flow rate can be determined. A pair of spaced apart electrodes can be used to produce the electrochemical pulse. In those instances where it is desired to measure a wide range of fluid flow rates a three electrode configuration in which the electrodes are spaced at unequal distances has been found to be desirable.

  11. INSTITUTE OF SPACE AND ATMOSPHERIC

    E-Print Network [OSTI]

    Saskatchewan, University of

    Gordon James Larry Newitt Tom McElroy David Kendall Malcolm Vant David Grier Senior Scientist, Space

  12. Space Data Systems (ISR-3)

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    Standard, including the processing and communications architecture, common hardware and software components, and its communications protocols Modular space payload architecture...

  13. Space-time diamonds

    E-Print Network [OSTI]

    Daiqin Su; T. C. Ralph

    2015-07-02

    We show that the particle number distribution of diamond modes, modes that are localised in a finite space-time region, are thermal for the Minkowski vacuum state of a massless scalar field, an analogue to the Unruh effect. The temperature of the diamond is inversely proportional to its size. An inertial observer can detect this thermal radiation by coupling to the diamond modes using an appropriate energy scaled detector. We further investigate the correlations between various diamonds and find that entanglement between adjacent diamonds dominates.

  14. Space Science and Applications

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantityBonneville Power AdministrationRobust,Field-effect Photovoltaics -7541C. TemperatureThousand CubicArchived1 Space Science and

  15. Multi-gap Resistive Plate Chambers as a Time-of-Flight System for the PHENIX Experiment

    SciTech Connect (OSTI)

    Velkovska, Julia

    2013-12-08

    In this project a Time-of-Flight detector based on multi-gap resistive plate chambers was built and installed for the PHENIX experiment at RHIC.

  16. Pathfinder flight of the Polarized Gamma-ray Observer (PoGOLite) in 2013

    E-Print Network [OSTI]

    Kawano, Takafumi

    2015-01-01

    The Polarized Gamma-ray Observer (PoGOLite) is a balloon-borne instrument that can measure polarization in the energy range 25--240 keV. The instrument adopts an array of well-type "phoswich" detectors in order to suppress backgrounds. Based on the anisotropy of Compton scattering angles resulting from polarized gamma-rays, the polarization of the observed source can be reconstructed. During July 12-26 of 2013, a successful near-circumpolar pathfinder flight was conducted from Esrange, Sweden, to Norilsk, Russia. During this two-week flight, several observations of the Crab were conducted. Here, we present the PoGOLite instrument and summarize the 2013 flight.

  17. System characterization and online mass property identification of the SPHERES formation flight testbed

    E-Print Network [OSTI]

    Berkovitz, Dustin S. (Dustin Scott)

    2008-01-01

    The National Aeronautics and Space Administration (NASA) and other entities in the aerospace industry have recently been considering distributed architectures for many space applications, such as space-based interferometry. ...

  18. Hilbert space of wormholes

    E-Print Network [OSTI]

    Luis J. Garay

    1993-06-01

    Wormhole boundary conditions for the Wheeler--DeWitt equation can be derived from the path integral formulation. It is proposed that the wormhole wave function must be square integrable in the maximal analytic extension of minisuperspace. Quantum wormholes can be invested with a Hilbert space structure, the inner product being naturally induced by the minisuperspace metric, in which the Wheeler--DeWitt operator is essentially self--adjoint. This provides us with a kind of probabilistic interpretation. In particular, giant wormholes will give extremely small contributions to any wormhole state. We also study the whole spectrum of the Wheeler--DeWitt operator and its role in the calculation of Green's functions and effective low energy interactions.

  19. Machian space quanta

    E-Print Network [OSTI]

    David W. Essex

    2015-01-25

    A new model for space and matter is obtained by joining every pair of point charges in the observable universe by an ethereal string. Positive gravitational potential energy in each string gives an attractive gravitational force due to the action of an energy conservation constraint. Newton's laws of motion are derived and inertia is explained in accordance with Mach's principle. The Machian string model gives a surprisingly simple way to understand the expansion history of the Universe. The decelerating expansion in the radiation era and the matter era is explained without using General Relativity and the transition from deceleration to acceleration is explained without the need to introduce a separate 'dark energy' component. The interaction between Machian strings gives a physical model for modified Newtonian dynamics (MOND) and is therefore an alternative to 'dark matter'.

  20. A NEW VIEW ON INTERSTELLAR DUST HIGH FIDELITY STUDIES OF INTERSTELLAR DUST ANALOGUE TRACKS IN STARDUST FLIGHT SPARE AEROGEL

    E-Print Network [OSTI]

    IN STARDUST FLIGHT SPARE AEROGEL F. Postberg, C. Allen, S. Bajt, H. A. Bechtel, J. Borg, F. Brenker, J the Stardust Mission exposed aerogel collector panels for a total of about 200 days to the stream - 30km/s] interstellar dust (ISD) analogues onto Stardust aerogel flight spares. This en- ables

  1. Laser photoionization time-of-flight mass spectrometry of nitrated polycyclic aromatic hydrocarbons and nitrated heterocyclic compounds. Master's thesis

    SciTech Connect (OSTI)

    Noyes, R.A.

    1993-01-01

    Partial Contents: Laser Desorption-Laser Photoionization Time-of-Flight Mass Spectrometry; Basic Principles of TOFMS; Factors Affecting Flight Time; Source of Broadening; Laser Desorption; Theory of Multiphoton Ionization: Application to Mass Spectrometry; Quantum Theory of MPI; Time-Dependent Perturbation Theory; Time-Dependent Coefficients; Probability of a Two-Photon Process; and Attributes of R2PI.

  2. No Prejudice in Space

    SciTech Connect (OSTI)

    Cotta, R.C.; Gainer, J.S.; Hewett, J.L.; Rizzo, T.G.; /SLAC

    2010-08-26

    We present a summary of recent results obtained from a scan of the 19-dimensional parameter space of the pMSSM and its implications for dark matter searches. We have generated a large set of points in parameter space (which we call 'models') for the 19-parameter CP-conserving pMSSM, where MFV has been assumed. We subjected these models to numerous experimental and theoretical constraints to obtain a set of {approx}68 K models which are consistent with existing data. We attempted to be somewhat conservative in our implementation of these constraints; in particular we only demanded that the relic density of the LSP not be greater than the measured value of {Omega}H{sup 2} for non-baryonic dark matter, rather than assuming that the LSP must account for the entire observed relic density. Examining the properties of the neutralinos in these models, we find that many are relatively pure gauge eigenstates with Higgsinos being the most common, followed by Winos. The relative prevalence of Higgsino and Wino LSPs leads many of our models to have a chargino as nLSP, often with a relatively small mass splitting between this nLSP and the LSP; this has important consequences in both collider and astroparticle phenomenology. We find that, in general, the LSP in our models provides a relatively small ({approx} 4%) contribution to the dark matter, however there is a long tail to this distribution and a substantial number of models for which the LSP makes up all or most of the dark matter. Typically these neutralinos are mostly Binos. Examining the signatures of our models in direct and indirect dark matter detection experiments, we find a wide range of signatures for both cases. In particular, we find a much larger range of WIMP-nucleon cross sections than is found in any particular model of SUSY-breaking. As these cross sections also enter the regions of parameter space suggested by non-SUSY models, it appears that the discovery of WIMPs in direct detection experiments might not be sufficient to determine the correct model of the underlying physics. As a first look at the signatures of these models in indirect detection experiments, we examined whether our models could explain the PAMELA excess in the positron to electron ratio at high energies. We find that there are models which fit the PAMELA data rather well, and some of these have significantly smaller boost factors than generally assumed for a thermal relic. The study of the pMSSM presents exciting new possibilities for SUSY phenomenology. The next few years will hopefully see important discoveries both in colliders and in satellite or ground-based astrophysical experiments. It is important that we follow the data and not our existing prejudices; hopefully this sort of relatively model-independent approach to collider and astrophysical phenomenology can be useful in this regard.

  3. Identification of High-Speed Rail Ballast Flight Risk Factors and Risk Mitigation Strategies

    E-Print Network [OSTI]

    Barkan, Christopher P.L.

    1 Identification of High-Speed Rail Ballast Flight Risk Factors and Risk Mitigation Strategies speed line, true high speed rail has seen an increasing success in those countries where such lines were speed rail (HSR) systems around the world during the past 50 years, one of the observed phenomena

  4. Modeling, Control, and Flight Testing of a Small Ducted Fan Aircraft

    E-Print Network [OSTI]

    Johnson, Eric N.

    1 Modeling, Control, and Flight Testing of a Small Ducted Fan Aircraft Eric N. Johnson* and Michael A. Turbe Georgia Institute of Technology, Atlanta, GA, 30332 Small ducted fan autonomous vehicles for the GTSpy, a small ducted fan autonomous vehicle based on the Micro Autonomous Systems' Helispy

  5. Toward a Better Understanding of Ducted Rotor Antitorque and Directional Control in Forward Flight

    E-Print Network [OSTI]

    Toward a Better Understanding of Ducted Rotor Antitorque and Directional Control in Forward Flight of ducted rotors in low-power, near-edgewise flow conditions are not well understood. Motivated by phenomena was initiated to use CFD to improve the understanding of the dynamic relationship between ducted rotor thrust

  6. Flight Test Evaluation of a Prototype Optical Instrument for Airborne Sense-and-Avoid Applications

    E-Print Network [OSTI]

    Hornsey, Richard

    Flight Test Evaluation of a Prototype Optical Instrument for Airborne Sense-and-Avoid Applications sense-and-avoid instrument was constructed from low-cost commercial off-the- shelf components 205 and the Bell 206 (intruder aircraft) were fully instrumented to record position and orientation

  7. Flight Testing a Real Time Implementation of a UAV Path Planner Using Direct Collocation

    E-Print Network [OSTI]

    Flight Testing a Real Time Implementation of a UAV Path Planner Using Direct Collocation Brian R by tracking a second UAV flying a predefined pattern. Finally, a method of commanding the observation vector ^s UAV sensor line of sight unit vector p Attraction point u UAV Control vector xt Target state

  8. UAV Formation Flight using 3D Potential Field Tobias Paul Thomas R. Krogstad Jan Tommy Gravdahl

    E-Print Network [OSTI]

    Gravdahl, Jan Tommy

    UAV Formation Flight using 3D Potential Field Tobias Paul Thomas R. Krogstad Jan Tommy Gravdahl ESG aerial vehicles (UAVs). Based on a virtual leader approach, combined with an extended local potential a group of UAVs based on a simplified small-scale helicopter, which is simulated in MATLABTM /Simulink

  9. Climate effects on the flight period of Lycaenid butterflies in Massachusetts

    E-Print Network [OSTI]

    Williams, Ernest H.

    Climate effects on the flight period of Lycaenid butterflies in Massachusetts Caroline A. Polgar a 2012 Accepted 16 December 2012 Keywords: Phenology Butterflies Climate change Museum records Citizen science a b s t r a c t The effect of climate change on the phenology of plants and birds of eastern North

  10. Roadmap: Aeronautics-Flight Technology-Bachelor of Science [AT-BS-AERN-FLGT

    E-Print Network [OSTI]

    Sheridan, Scott

    Roadmap: Aeronautics-Flight Technology-Bachelor of Science [AT-BS-AERN-FLGT] College of Applied This roadmap is a recommended semester-by-semester plan of study for this major. However, courses Resource Management 2 Offered in fall only AERN 45721 Crew Resource Management Laboratory 1 #12;Roadmap

  11. NIST Report to the FBI: Plex-ID Electrospray Time-of-Flight Mass

    E-Print Network [OSTI]

    1 NIST Report to the FBI: Plex-ID Electrospray Time-of-Flight Mass Spectrometer for Mitochondrial. John Butler (NIST) Dr. Thomas Callaghan (FBI) Eric Pokorak (FBI) Points of view in this document of Investigation (FBI). Certain commercial equipment, instruments, and materials are identified in order to specify

  12. DIGITAL DATA ACQUISITION SYSTEM FOR TIME OF FLIGHT NEUTRON BEAM MEASUREMENTS

    E-Print Network [OSTI]

    Danon, Yaron

    , 12180, saglif@rpi.edu INTRODUCTION A system for neutron scattering measurements is under developmentDIGITAL DATA ACQUISITION SYSTEM FOR TIME OF FLIGHT NEUTRON BEAM MEASUREMENTS Frank J. Saglime III at the RPI LINAC [1]. The system is design to provide additional differential scattering data to improve upon

  13. 2007 Instrument Procedures Handbook; Chapter 5 Approach Authors: US Department of Transportation, Federal Aviation Administration (Flight

    E-Print Network [OSTI]

    Kaber, David B.

    , Federal Aviation Administration (Flight Procedures Standards Branch) From: www.faa.gov/library/manuals/aviation with weather around airports because it #12;influences the approaches they can implement, the amount of fuel used, and alternate approach planning. AIRPLANE PERFORMANCE OPERTING LIMITATIONS (Page 5-6) All

  14. FUNCTIONAL COMPLEXITY FAILURES AND AUTOMATION SURPRISES: THE MYSTERIOUS CASE OF CONTROLLED FLIGHT INTO STALL (CFIS)

    E-Print Network [OSTI]

    1 FUNCTIONAL COMPLEXITY FAILURES AND AUTOMATION SURPRISES: THE MYSTERIOUS CASE OF CONTROLLED FLIGHT of behaviors of the automation functions. There were no consistent: failures that triggered the events (e.g. sensor failures), effects of triggering events on the automation (e.g. mode change), or commands issued

  15. Complete CFD analysis of a Velocity XL-5 RG with flight-test verification 

    E-Print Network [OSTI]

    Schouten, Shane Michael

    2008-10-10

    in the wing. Therefore, it is necessary to understand the influence the canard and the impact of its wake on the wing of the aircraft before any in-depth aerodynamic research could be completed on the aircraft. A combination of in-flight measurements...

  16. GLOMAP Approach for Nonlinear System Identification of Aircraft Dynamics Using Flight Data

    E-Print Network [OSTI]

    Valasek, John

    GLOMAP Approach for Nonlinear System Identification of Aircraft Dynamics Using Flight Data Monika model dynamics are assumed to be perturbed by a nonlinear term which represents the system accurate behavior. Nonlinear system identification of aircraft dynamics is a comparitively new and still

  17. Texas Tech University Pre-Flight Checklist for TTU Web Pages

    E-Print Network [OSTI]

    Rock, Chris

    Texas Tech University Pre-Flight Checklist for TTU Web Pages In order to help ensure that all Texas Tech University web pages are created and maintained in accordance with the TTU Web Guidelines-browser compatibility Accessibility Ensure pages comply with the Texas Administrative Code (TAC) §206, State Web

  18. The Fight and Flight Responses of Crickets Depleted of Biogenic Amines

    E-Print Network [OSTI]

    Hofmann, Hans A.

    The Fight and Flight Responses of Crickets Depleted of Biogenic Amines Paul A. Stevenson, Hans A or submissive behaviors. AMT-treated crickets could normally only be brought to fight by coaxing. Though capable metabolic body functions for the prospective fight, whereas the central nervous noradrenergic sys- tem

  19. Data-driven Control of Flapping Flight EUNJUNG JU and JUNGDAM WON and JEHEE LEE

    E-Print Network [OSTI]

    Lee, Jehee

    in high-speed videos (see Figure 3). 3.2 System Overview Our flight control system consists of three main graphs that vary in its shape, amplitude, and phase (see Figure 5). We use a parametrized wingbeat model the controller from the first phase for random control tasks. In Figure 10, we plotted the outputs (P

  20. Flight Path and Wing Optimization of Lithium-Air Battery Powered Passenger Aircraft

    E-Print Network [OSTI]

    Alonso, Juan J.

    in the design of electrically-driven aircraft, particularly in the case of fuel cells and batteries.5­7 One to implement vis. a vis. fuel cells, in particular, liquid hydrogen fuel cells. However, present-day batteryFlight Path and Wing Optimization of Lithium-Air Battery Powered Passenger Aircraft J. Michael Vegh

  1. Laser desorption time-of-flight mass spectrometer DNA analyzer. Final report

    SciTech Connect (OSTI)

    Chen, C.H.W.; Martin, S.A.

    1997-02-01

    The objective of this project is the development of a laser desorption time-of-flight mass spectrometer DNA analyzer which can be broadly used for biomedical research. Tasks include: pulsed ion extraction to improve resolution; two-component matrices to enhance ionization; and solid phase DNA purification.

  2. Using Simulations To Determine The Energy Resolution Function Of Neutron Time-Of-Flight Experiments

    E-Print Network [OSTI]

    Danon, Yaron

    and their contribution to the understanding of nuclear models and interaction theory. At the Rensselaer Gaerttner LinearUsing Simulations To Determine The Energy Resolution Function Of Neutron Time-Of- Flight INTRODUCTION High resolution nuclear data are important in their application in neutron transport calculations

  3. Development of an Adaptive Flap/Flaperon Flight Control System with Shape Memory Alloy Actuation

    E-Print Network [OSTI]

    Sinn, Thomas

    2010-06-09

    Edge Part in Tool ...................................................................................... 64 Figure 59: Applied Strain Gages with Connection Wires ........................................................ 65 Figure 60: Stretching... function of temperature. The application of adaptive materials in aerospace structures seems to be perfect because of their low weight and part count compared to conventional aerospace structures. Due to the fact that several different flight regimes...

  4. Lyapunov Vector Fields for Autonomous UAV Flight Control1 Dale A. Lawrence2

    E-Print Network [OSTI]

    Frew, Eric W.

    Lyapunov Vector Fields for Autonomous UAV Flight Control1 Dale A. Lawrence2 , Eric. W. Frew3 that incorporate Lyapunov stability properties to produce simple, globally stable vector fields in 3D. Use of the vector field is considered, using Lyapunov techniques to show global stability of heading and path

  5. LETTER TO THE EDITOR Levy Flights: Transitions and Meta-Stability

    E-Print Network [OSTI]

    Imkeller, Peter

    values increase as a power - of the noise intensity . This allows to obtain meta- stability results of financial markets [7]. L´evy flights also naturally appear in particle evolutions along polymer chains [8, 9 increments and marginals with symmetric stable laws of index (0, 2). The Fourier transform of the marginal

  6. Neutron-induced fission measurements at the time-of-flight facility nELBE

    SciTech Connect (OSTI)

    Kögler, T. [Helmholtz-Zentrum Dresden-Rossendorf, Dresden (Germany); Technische Univ. Dresden, Dresden (Germany); Beyer, R. [Helmholtz-Zentrum Dresden-Rossendorf, Dresden (Germany); Junghans, A. R. [Helmholtz-Zentrum Dresden-Rossendorf, Dresden (Germany); Massarczyk, R. [Helmholtz-Zentrum Dresden-Rossendorf, Dresden (Germany); Los Alamos National Lab. (LANL), Los Alamos, NM (United States); Schwengner, R. [Helmholtz-Zentrum Dresden-Rossendorf, Dresden (Germany); Wagner, A. [Helmholtz-Zentrum Dresden-Rossendorf, Dresden (Germany)

    2015-01-01

    Neutron-induced fission of ˛?˛Pu is studied at the photoneutron source nELBE. The relative fast neutron fission cross section was determined using actinide fission chambers in a time-of-flight experiment. A good agreement of present nuclear data with evalua- tions has been achieved in the range of 100 keV to 10 MeV.

  7. 1182 J. GUIDANCE, VOL. 19, NO. 5: ENGINEERING NOTES Fig. 2 Fixed and optimized flight paths.

    E-Print Network [OSTI]

    Singh, Tarunraj

    and optimized flight paths. Conclusion A simple guidance law for operation of dual-fuel SSTO launch vehicles hasbeen developed andused to determine the optimal value of the transition Mach number from dual fuel higher dynamic pressure than the fixed, particularly in dual-fuel mode. In the future, the guidance

  8. Targeted Autonomous Indoor Flight of a Rotary-Wing MAV Svetlana Potyagaylo

    E-Print Network [OSTI]

    Kanza, Yaron

    Targeted Autonomous Indoor Flight of a Rotary-Wing MAV Svetlana Potyagaylo PhD Student Faculty of Aerospace Engineering svetap@tx.technion.ac.il Omri Rand Professor Faculty of Aerospace Engineering omri for Autonomous Rotary-Wing Micro Aerial Vehicles (RW MAVs) in indoor GPS-denied environments. In such missions

  9. Deformed wing virus and drone mating flights in the honey bee (Apis mellifera): implications for sexual

    E-Print Network [OSTI]

    Paxton, Robert

    Deformed wing virus and drone mating flights in the honey bee (Apis mellifera): implications clear evidence for the occurrence of high DWV titres in the endophallus of sexually mature drones collected from drone congregation areas (DCAs). Furthermore, the endophallus DWV titres of drones collected

  10. Neutron-induced fission measurements at the time-of-flight facility nELBE

    DOE Public Access Gateway for Energy & Science Beta (PAGES Beta)

    Kögler, T.; Beyer, R.; Junghans, A. R.; Massarczyk, R.; Schwengner, R.; Wagner, A.

    2015-05-18

    Neutron-induced fission of ˛?˛Pu is studied at the photoneutron source nELBE. The relative fast neutron fission cross section was determined using actinide fission chambers in a time-of-flight experiment. A good agreement of present nuclear data with evalua- tions has been achieved in the range of 100 keV to 10 MeV.

  11. Design and implementation of a robust and nonlinear flight control system for an unmanned helicopter

    E-Print Network [OSTI]

    Benmei, Chen

    : Available online 4 March 2011 Keywords: Unmanned aerial vehicles Unmanned systems Nonlinear flight dynamics driving to device operation management. Among various unmanned aerial vehicles (UAVs), small. Software systems for unmanned vehicles are required to per- form multi-level tasks, such as from hardware

  12. Bio-Inspired Visuomotor Convergence in Navigation and Flight Control Systems

    E-Print Network [OSTI]

    Murray, Richard M.

    , extraction of global retinal motion cues through computationally efficient wide-field integration process. A fundamental principle contributing to this unparalleled behavior is rapid processing and convergence of visual sensory information to flight motor commands via spatial wide-field integration, accomplished by retinal

  13. Entropic Gravity in Rindler Space

    E-Print Network [OSTI]

    Edi Halyo

    2011-04-13

    We show that Rindler horizons are entropic screens and gravity is an entropic force in Rindler space by deriving the Verlinde entropy formula from the focusing of light due to a mass close to the horizon. Consequently, gravity is also entropic in the near horizon regions of Schwarzschild and de Sitter space-times. In different limits, the entropic nature of gravity in Rindler space leads to the Bekenstein entropy bound and the uncertainty principle.

  14. Space Instrument Realization (ISR-5)

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    design, and fabrication support to all aspects of mechanical and electronic assemblies Mechanical analysis with a focus on space environment-radiation, thermal, vibration...

  15. TANK SPACE ALTERNATIVES ANALYSIS REPORT

    SciTech Connect (OSTI)

    TURNER DA; KIRCH NW; WASHENFELDER DJ; SCHAUS PS; WODRICH DD; WIEGMAN SA

    2010-04-27

    This report addresses the projected shortfall of double-shell tank (DST) space starting in 2018. Using a multi-variant methodology, a total of eight new-term options and 17 long-term options for recovering DST space were evaluated. These include 11 options that were previously evaluated in RPP-7702, Tank Space Options Report (Rev. 1). Based on the results of this evaluation, two near-term and three long-term options have been identified as being sufficient to overcome the shortfall of DST space projected to occur between 2018 and 2025.

  16. Portfolio Manager Space Type Discussion

    Broader source: Energy.gov [DOE]

    This presentation, given through the DOE's Technical Assistance Program (TAP), provides a discussion about space/type in regards to the Portfolio Manager Initiative.

  17. Radioisotopes: Energy for Space Exploration

    SciTech Connect (OSTI)

    Carpenter, Bob; Green, James; Bechtel, Ryan

    2011-01-01

    Through a strong partnership between the Energy Department's office of Nuclear Energy and NASA, Radioisotope Power Systems have been providing the energy for deep space exploration.

  18. Flat space physics from holography

    E-Print Network [OSTI]

    Bousso, Raphael

    2009-01-01

    thermodynamics in black hole physics. Phys. Rev. D 9, 3292 (LBNL-53861 Flat space physics from holography RaphaelBousso Center for Theoretical Physics, Department of Physics

  19. Linear Programming and Kantorovich Spaces

    E-Print Network [OSTI]

    S. Kutateladze

    2009-05-08

    This is a brief overview of the life of Leonid Kantorovich (1912--1986) and his contribution to the fields of linear programming and ordered vector spaces.

  20. Space Instrument Realization (ISR-5)

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    and fabrication (NASA-certified) assembly Parts inventory database based on "pcMRP" software package Quality assurance System test and integration Space systems engineering...

  1. Radioisotopes: Energy for Space Exploration

    ScienceCinema (OSTI)

    Carpenter, Bob; Green, James; Bechtel, Ryan

    2013-05-29

    Through a strong partnership between the Energy Department's office of Nuclear Energy and NASA, Radioisotope Power Systems have been providing the energy for deep space exploration.

  2. Portfolio Manager Space Type Discussion

    Broader source: Energy.gov [DOE]

    This presentation, given through the DOE's Technical Assitance Program (TAP), provides a discussion about space/type in regards to the Portfolio Manager Initiative.

  3. CAPTAIN DAVID M. ROGERS Captain David M. Rogers is the Recruiting Flight Commander

    E-Print Network [OSTI]

    Advisor and Ground Systems Engineer, 1st Space Operations Squadron, Schriever AFB, CO 3. 2012 ­ 2014

  4. Building America Webinar: Retrofitting Central Space Conditioning...

    Energy Savers [EERE]

    Webinar: Retrofitting Central Space Conditioning Strategies for Multifamily Buildings - Control strategies to improve hydronic space heating performance Building America Webinar:...

  5. Constrained space camera assembly

    DOE Patents [OSTI]

    Heckendorn, F.M.; Anderson, E.K.; Robinson, C.W.; Haynes, H.B.

    1999-05-11

    A constrained space camera assembly which is intended to be lowered through a hole into a tank, a borehole or another cavity is disclosed. The assembly includes a generally cylindrical chamber comprising a head and a body and a wiring-carrying conduit extending from the chamber. Means are included in the chamber for rotating the body about the head without breaking an airtight seal formed therebetween. The assembly may be pressurized and accompanied with a pressure sensing means for sensing if a breach has occurred in the assembly. In one embodiment, two cameras, separated from their respective lenses, are installed on a mounting apparatus disposed in the chamber. The mounting apparatus includes means allowing both longitudinal and lateral movement of the cameras. Moving the cameras longitudinally focuses the cameras, and moving the cameras laterally away from one another effectively converges the cameras so that close objects can be viewed. The assembly further includes means for moving lenses of different magnification forward of the cameras. 17 figs.

  6. Physics in discrete spaces (A): Space-Time organization

    E-Print Network [OSTI]

    P. Peretto

    2010-12-29

    We put forward a model of discrete physical space that can account for the structure of space- time, give an interpretation to the postulates of quantum mechanics and provide a possible explanation to the organization of the standard model of particles.

  7. National Aeronautics and Space Administration space launch system

    E-Print Network [OSTI]

    Rathbun, Julie A.

    into the solar system ­ finding potential resources, develop- ing new technologies, and discovering answersNational Aeronautics and Space Administration NASAfacts space launch system Building America's Next to reach further into our solar system. However, if needed, SLS will support backup trans- portation

  8. Finite Linear Spaces, Plane Geometries, Hilbert spaces and Finite Phase Space

    E-Print Network [OSTI]

    M. Revzen; A. Mann

    2015-08-03

    Finite plane geometry is associated with finite dimensional Hilbert space. The association allows mapping of q-number Hilbert space observables to the c-number formalism of quantum mechanics in phase space. The mapped entities reflect geometrically based line-point interrelation. Particularly simple formulas are involved when use is made of mutually unbiased bases (MUB) representations for the Hilbert space entries. The geometry specifies a point-line interrelation. Thus underpinning d-dimensional Hilbert space operators (resp. states) with geometrical points leads to operators termed "line operators" underpinned by the geometrical lines. These "line operators", $\\hat{L}_j;$ (j designates the line) form a complete orthogonal basis for Hilbert space operators. The representation of Hilbert space operators in terms of these operators form the phase space representation of the d-dimensional Hilbert space. The "line operators" (resp. "line states") are studied in detail. The paper aims at self sufficiency and to this end all relevant notions are explained herewith.

  9. Space Science : Atmosphere Greenhouse Effect

    E-Print Network [OSTI]

    Johnson, Robert E.

    Space Science : Atmosphere Greenhouse Effect Part-5a Solar + Earth Spectrum IR Absorbers Grey Atmosphere Greenhouse Effect #12;Radiation: Solar and Earth Surface B"(T) Planck Ideal Emission Integrate and it emits Note: heat balance Fvis( = Fout = Te 4 z #12;(simple Greenhouse cont.) 0 1 2 3 4 Ground Space Top

  10. National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Rathbun, Julie A.

    commercial and international partner transportation services to the International Space Station. Designed Administrator Initial Lift Capability 70 Tonnes (t) More than Double Any Operational Vehicle Today Crew orbit, continuing America's human exploration of space. Evolved Lift Capability 130t More than Any Past

  11. Space Telescope Programs Hubble Observatory

    E-Print Network [OSTI]

    Colorado at Boulder, University of

    Certifications required for all raw materials ­ Shelf Life (Polymerics) materials date controlled by QA · DesignsSpace Telescope Programs Hubble Observatory HST-COS FUV PER 11/8/00 FUV Detector System Materials;Space Telescope Programs Hubble Observatory HST-COS FUV PER 11/8/00 Materials and Processes · Materials

  12. National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Rathbun, Julie A.

    National Aeronautics and Space Administration The Vision for Space Exploration February 2004 #12 #12;Message from the NASA Administrator Dear Reader, With last year's budget, NASA released a new of careful deliberations within the Administration. This plan does not undertake exploration merely

  13. Nonlinear classification of Banach spaces 

    E-Print Network [OSTI]

    Randrianarivony, Nirina Lovasoa

    2005-11-01

    We study the geometric classi?cation of Banach spaces via Lipschitz, uniformly continuous, and coarse mappings. We prove that a Banach space which is uniformly homeomorphic to a linear quotient of lp is itself a linear quotient of lp when p<2...

  14. How Common are Noise Sources on the Crash Arc of Malaysian Flight 370

    SciTech Connect (OSTI)

    Fenimore, Edward E.; Kunkle, Thomas David; Stead, Richard J.

    2014-10-21

    Malaysian Flight 370 disappeared nearly without a trace. Besides some communication handshakes to the INMASAT satellite, the Comprehensive Test Ban Treaty monitoring system could have heard the aircraft crash into the southern Indian Ocean. One noise event from Cape Leeuwin has been suggested by Stead as the crash and occurs within the crash location suggested by Kunkle at el. We analyze the hydrophone data from Cape Leeuwin to understand how common such noise events are on the arc of possible locations where Malaysian Flight 370 might have crashed. Few other noise sources were found on the arc. The noise event found by Stead is the strongest. No noise events are seen within the Australian Transportation Safety Board (ATSB) new search location until the 10th strongest event, an event which is very close to the noise level.

  15. Data acquisition system with pulse height capability for the TOFED time-of-flight neutron spectrometer

    SciTech Connect (OSTI)

    Chen, Z. J.; Peng, X. Y.; Zhang, X.; Du, T. F.; Hu, Z. M.; Cui, Z. Q.; Ge, L. J.; Xie, X. F.; Yuan, X.; Li, X. Q.; Zhang, G. H.; Chen, J. X.; Fan, T. S., E-mail: tsfan@pku.edu.cn [School of Physics and State Key Laboratory of Nuclear Physics and Technology, Peking University, Beijing 100871 (China); Gorini, G.; Nocente, M.; Tardocchi, M. [Dipartimento di Fisica, Universitŕ di Milano-Bicocca, Milano, Piazza della Scienza 3, 20126 Milano (Italy); Istituto di Fisica del Plasma “P. Caldirola”, EURATOM-ENEA-CNR Association, Via Cozzi 53, 20125 Milano (Italy); Hu, L. Q.; Zhong, G. Q.; Lin, S. Y.; Wan, B. N. [Institute of Plasma Physics, Chinese Academy of Sciences, Hefei 230031, Anhui (China)

    2014-11-15

    A new time-of-flight neutron spectrometer TOFED has been constructed for installation at Experimental Advanced Superconducting Tokamak. A data acquisition system combining measurements of flight time and energy from the interaction of neutrons with the TOFED scintillators has been developed. The data acquisition system can provide a digitizing resolution better than 1.5% (to be compared with the >10% resolution of the recoil particle energy in the plastic scintillators) and a time resolution <1 ns. At the same time, it is compatible with high count rate event recording, which is an essential feature to investigate phenomena occurring on time scales faster than the slowing down time (?100 ms) of the beam ions in the plasma. Implications of these results on the TOFED capability to resolve fast ion signatures in the neutron spectrum from EAST plasmas are discussed.

  16. Detection system for high-resolution gamma radiation spectroscopy with neutron time-of-flight filtering

    DOE Patents [OSTI]

    Dioszegi, Istvan; Salwen, Cynthia; Vanier, Peter

    2014-12-30

    A .gamma.-radiation detection system that includes at least one semiconductor detector such as HPGe-Detector, a position-sensitive .alpha.-Detector, a TOF Controller, and a Digitizer/Integrator. The Digitizer/Integrator starts to process the energy signals of a .gamma.-radiation sent from the HPGe-Detector instantly when the HPGe-Detector detects the .gamma.-radiation. Subsequently, it is determined whether a coincidence exists between the .alpha.-particles and .gamma.-radiation signal, based on a determination of the time-of-flight of neutrons obtained from the .alpha.-Detector and the HPGe-Detector. If it is determined that the time-of-flight falls within a predetermined coincidence window, the Digitizer/Integrator is allowed to continue and complete the energy signal processing. If, however, there is no coincidence, the Digitizer/Integrator is instructed to be clear and reset its operation instantly.

  17. Polychronous Interpretation of Synoptic, a Domain Specific Modeling Language for Embedded Flight-Software

    E-Print Network [OSTI]

    Besnard, L; Ouy, J; Talpin, J -P; Bodeveix, J -P; Cortier, A; Pantel, M; Strecker, M; Garcia, G; Rugina, A; Buisson, J; Dagnat, F

    2010-01-01

    The SPaCIFY project, which aims at bringing advances in MDE to the satellite flight software industry, advocates a top-down approach built on a domain-specific modeling language named Synoptic. In line with previous approaches to real-time modeling such as Statecharts and Simulink, Synoptic features hierarchical decomposition of application and control modules in synchronous block diagrams and state machines. Its semantics is described in the polychronous model of computation, which is that of the synchronous language Signal.

  18. NASA 36.286 Flight Summary SDO EVE Calibration Rocket flown on June 23, 2012

    E-Print Network [OSTI]

    Mojzsis, Stephen J.

    NASA 36.286 Flight Summary SDO EVE Calibration Rocket flown on June 23, 2012 (only quicklook data degradation of about 10%/year is due to hydrocarbon contaminates. #12;Summary of NASA 36.286 Results All EVE SAM X-ray SDO AIA 17.1 nm SDO HMI Mag. Fields #12;NASA 36.286: MEGS-A (5-37 nm) MEGS-A has dual

  19. Genetic icing effects on forward flight performance of a model helicopter rotor 

    E-Print Network [OSTI]

    Tinetti-Sanchez, Ana Fiorella

    1987-01-01

    introduces decrements in performance caused by leading edge separation regions and increased surface roughness, In addition to the expected changes in aerodynamic forces caused by var- iations in test Reynolds number, forward flight data seemed to be in... coefficient CT - thrust coefficient CY - Y-force coefficient c - blade chord c~ - section lift coefficient cd - section drag coefficient D - drag (wind axis) De - equivalent drag Dp - profile drag FM - Figure of Merit F - section radial aerodynamic...

  20. Innovation in the design and development of a commercial flight termination system

    E-Print Network [OSTI]

    Kwak, Eugene

    2013-01-01

    With the ramp up of commercial spaceflight over the last decade with the assistance of the US Government and NASA, commercial spaceflight companies such as Space Exploration Technologies (SpaceX) and Orbital Sciences have ...

  1. Nanometer scale elemental analysis in the helium ion microscope using time of flight spectrometry

    E-Print Network [OSTI]

    Klingner, Nico; Hlawacek, Gregor; von Borany, Johannes; Notte, John; Huang, Jason; Facsko, Stefan

    2015-01-01

    Time of flight Rutherford backscattering spectrometry (ToF-RBS) was successfully implemented in a helium ion microscope (HIM). Its integration introduces the ability to perform laterally resolved elemental analysis as well as elemental depth profiling on the nm scale. A lateral resolution of $\\leq$ 54 nm and an energy resolution of $\\Delta E \\leq$ 1.5 keV $(\\Delta E/E=5.4\\%)$ are achieved. By using the energy of the backscattered particles for contrast generation, we introduce a new imaging method to the HIM allowing direct elemental mapping as well as local spectrometry. In addition laterally resolved time of flight secondary ion mass spectrometry (ToF-SIMS) can be performed with the same setup. Time of flight is implemented by pulsing the primary ion beam. This is achieved in a cost effective and minimal invasive way that does not influence the high resolution capabilities of the microscope when operating in standard secondary electron (SE) imaging mode. This technique can thus be easily adapted to existing...

  2. CRAD, Confined Spaces Assessment Plan

    Broader source: Energy.gov [DOE]

    This assessment provides a basis for evaluating the safety effectiveness of the contractor’s confined or enclosed spaces procedure, and for establishing compliance with DOE and OSHA requirements.

  3. National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Guattery, Steve

    National Aeronautics and Space Administration Langley Research Center Hampton, Virginia 23681, Hampton, VA 23681­0001 (email: smg@icase.edu). This research was supported by the National Aeronautics

  4. I. Cover Page Ubiquitous Smart Spaces

    E-Print Network [OSTI]

    Abowd, Gregory D.

    I. Cover Page Ubiquitous Smart Spaces Topic Area: Smart Spaces Gregory Abowd, Chris Atkeson, Irfan. Ubiquitous Smart Spaces II.1 Innovative Capability Envisioned The next revolutionary advance in smart spaces research is to create and experiment with ubiquitous smart spaces. Current research has created isolated

  5. Dr. David Kortenkamp NASA Johnson Space Center

    E-Print Network [OSTI]

    Kortenkamp, David

    Dr. David Kortenkamp NASA Johnson Space Center Dr. David Kortenkamp NASA Johnson Space Center Intelligent Robots for Space Applications Intelligent Robots for Space Applications Dr. David Kortenkamp NASA Johnson Space Center/Metrica Inc. Houston TX 77058 kortenkamp@jsc.nasa.gov http

  6. Nuclear Propulsion in Space (1968)

    SciTech Connect (OSTI)

    2012-06-23

    Project NERVA was an acronym for Nuclear Engine for Rocket Vehicle Application, a joint program of the U.S. Atomic Energy Commission and NASA managed by the Space Nuclear Propulsion Office (SNPO) at the Nuclear Rocket Development Station in Jackass Flats, Nevada U.S.A. Between 1959 and 1972, the Space Nuclear Propulsion Office oversaw 23 reactor tests, both the program and the office ended at the end of 1972.

  7. Nuclear Propulsion in Space (1968)

    ScienceCinema (OSTI)

    None

    2014-06-17

    Project NERVA was an acronym for Nuclear Engine for Rocket Vehicle Application, a joint program of the U.S. Atomic Energy Commission and NASA managed by the Space Nuclear Propulsion Office (SNPO) at the Nuclear Rocket Development Station in Jackass Flats, Nevada U.S.A. Between 1959 and 1972, the Space Nuclear Propulsion Office oversaw 23 reactor tests, both the program and the office ended at the end of 1972.

  8. Guaranteed margins and performance for an adaptive flight control system and application on the X-15 research airplane

    E-Print Network [OSTI]

    Dydek, Zachary Thompson

    2007-01-01

    The design tools developed for use with linear controllers such as gain and phase margins do not apply to nonlinear control architectures such as adaptive control. For decades, flight control engineers have used these tools ...

  9. IEEE TRANSACTIONS ON NUCLEAR SCIENCE, VOL. 50, NO. 3, JUNE 2003 421 Optimal Nonlinear Line-of-Flight Estimation in

    E-Print Network [OSTI]

    Zeevi, Yehoshua Y. "Josh"

    --Artificial neural network, emission tomography, gamma camera, scintillation detector. I. INTRODUCTION DETECTION-of-Flight Estimation in Positron Emission Tomography Alexander M. Bronstein, Michael M. Bronstein, Michael Zibulevsky tomography using thick scintillation crys- tals. Parallax effect and multiple Compton interactions

  10. Characterization of a pulsed beam Time-of-Flight system for medium energy He+ and C+ backscattering spectrometry 

    E-Print Network [OSTI]

    Thompson, Kelly

    1994-01-01

    Efficiencies of a microchannel plate detector for medium energy helium and carbon ions were determined using a recently developed time of flight technique for near surface analysis by medium energy ion scattering. This technique utilizes a pulsed...

  11. Development of a variable-temperature ion mobility/ time-of-flight mass spectrometer for separation of electronic isomers 

    E-Print Network [OSTI]

    Verbeck, Guido Fridolin

    2005-08-29

    The construction of a liquid nitrogen-cooled ion mobility spectrometer coupled with time-of-flight mass spectrometry was implemented to demonstrate the ability to discriminate between electronic isomers. Ion mobility allows for the separation...

  12. Development of tandem time-of-flight instrumentation for the examination of prompt photodissociation of peptides using 193-nm radiation 

    E-Print Network [OSTI]

    Morgan, Joseph William

    2006-04-12

    The design and incorporation of a decelerating/accelerating cell into a reflectron time-of-flight mass spectrometer is described for the examination of promptly-formed photodissociation products of peptide ions. The analytical utility of prompt 193...

  13. Characterisation of individual airborne particles by using aerosol time-of-flight mass spectrometry (ATOFMS) at Mace Head, Ireland, 

    E-Print Network [OSTI]

    Dall'Osto, Manuel; Beddows, David C S; Kinnersley, Robert P; Harrison, Roy M; Donovan, Robert J; Heal, Mathew R

    2004-01-01

    An aerosol time-of-flight mass spectrometer was deployed at Mace Head (Ireland) during August 2002. The measurements provide qualitative chemical composition and size distribution (0.3–3 ?m) information for single ...

  14. Dynamical 3-Space: Emergent Gravity

    E-Print Network [OSTI]

    Reginald T Cahill

    2011-02-16

    The laws of gravitation devised by Newton, and by Hilbert and Einstein, have failed many experimental and observational tests, namely the bore hole g anomaly, flat rotation curves for spiral galaxies, supermassive black hole mass spectrum, uniformly expanding universe, cosmic filaments, laboratory G measurements, galactic EM bending, precocious galaxy formation,.. The response has been the introduction of the new epicycles: ``dark matter", ``dark energy", and others. To understand gravity we must restart with the experimental discoveries by Galileo, and following a heuristic argument we are led to a uniquely determined theory of a dynamical 3-space. That 3-space exists has been missed from the beginning of physics, although it was 1st directly detected by Michelson and Morley in 1887. Uniquely generalising the quantum theory to include this dynamical 3-space we deduce the response of quantum matter and show that it results in a new account of gravity, and explains the above anomalies and others. The dynamical theory for this 3-space involves G, which determines the dissipation rate of space by matter, and alpha, which experiments and observation reveal to be the fine structure constant. For the 1st time we have a comprehensive account of space and matter and their interaction - gravity.

  15. Configuration Spaces in Fundamental Physics

    E-Print Network [OSTI]

    Edward Anderson

    2015-05-13

    I consider configuration spaces for $N$-body problems, gauge theories and for GR in both geometrodynamical and Ashtekar variables forms, including minisuperspace and inhomogeneous perturbations thereabout in the former case. These include many interesting spaces of shapes (with and without whichever of local or global notions of scale). In considering reduced configuration spaces, stratified manifolds arise. Three strategies to deal with these are `excise', `unfold' and `accept'. I show that spaces of triangles arising from various interpretations of 3-body problems already serve as model arena for all three. I furthermore argue in favour of the `accept' strategy on relational grounds. Sheaf methods then become relevant in this case, as does the stratifold construct that pairs some well-behaved stratified manifolds with sheaves. I apply arguing against `excise' and `unfold' to GR's superspace and thin sandwich, and to the removal of collinear configurations in mechanics. Non-redundant configurations are also useful in providing more accurate names for various spaces and theories. I also cover notions of distance between shapes, that some perturbative midisuperspace configuration spaces are simple and similar to minisuperspace ones, and similarities between CS (conformal superspace) and CS + V (including the global spatial volume).

  16. Small Space Heater Basics | Department of Energy

    Energy Savers [EERE]

    Small Space Heater Basics Small Space Heater Basics August 19, 2013 - 10:38am Addthis Small space heaters, also called portable heaters, are typically used when the main heating...

  17. Oxidation Behavior of In-Flight Molten Aluminum Droplets in the Twin-Wire Electric Arc Thermal Spray Process

    SciTech Connect (OSTI)

    Donna Post Guillen; Brian G. Williams

    2005-05-01

    This paper examines the in-flight oxidation of molten aluminum sprayed in air using the twin-wire electric arc (TWEA) thermal spray process. The oxidation reaction of aluminum in air is highly exothermic and is represented by a heat generation term in the energy balance. Aerodynamic shear at the droplet surface enhances the amount of in-flight oxidation by: (1) promoting entrainment and mixing of the surface oxides within the droplet, and (2) causing a continuous heat generation effect that increases droplet temperature over that of a droplet without internal circulation. This continual source of heat input keeps the droplets in a liquid state during flight. A linear rate law based on the Mott-Cabrera theory was used to estimate the growth of the surface oxide layer formed during droplet flight. The calculated oxide volume fraction of an average droplet at impact agrees well with the experimentally determined oxide content for a typical TWEA-sprayed aluminum coating, which ranges from 3.3 to 12.7%. An explanation is provided for the elevated, nearly constant surface temperature (~ 2000 oC) of the droplets during flight to the substrate and shows that the majority of oxide content in the coating is produced during flight, rather than after deposition.

  18. Building America Webinar: High Performance Space Conditioning...

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    II - Design Options for Locating Ducts within Conditioned Space Building America Webinar: High Performance Space Conditioning Systems, Part II - Design Options for Locating Ducts...

  19. Building America Webinar: High Performance Space Conditioning...

    Energy Savers [EERE]

    Webinar: High Performance Space Conditioning Systems, Part II - Air Distribution Retrofit Strategies for Affordable Housing Building America Webinar: High Performance Space...

  20. Total Space Heating Water Heating Cook-

    Gasoline and Diesel Fuel Update (EIA)

    Released: September, 2008 Total Space Heating Water Heating Cook- ing Other Total Space Heating Water Heating Cook- ing Other All Buildings* ... 1,602 1,397...

  1. Total Space Heating Water Heating Cook-

    Gasoline and Diesel Fuel Update (EIA)

    Energy Consumption Survey: Energy End-Use Consumption Tables Total Space Heating Water Heating Cook- ing Other Total Space Heating Water Heating Cook- ing Other All...

  2. Total Space Heating Water Heating Cook-

    Gasoline and Diesel Fuel Update (EIA)

    Released: September, 2008 Total Space Heating Water Heating Cook- ing Other Total Space Heating Water Heating Cook- ing Other All Buildings ... 2,037...

  3. Total Space Heating Water Heating Cook-

    Gasoline and Diesel Fuel Update (EIA)

    Released: September, 2008 Total Space Heating Water Heating Cook- ing Other Total Space Heating Water Heating Cook- ing Other All Buildings* ... 1,870 1,276...

  4. Space Conditioning Standing Technical Committee Strategic Plan...

    Office of Energy Efficiency and Renewable Energy (EERE) Indexed Site

    Space Conditioning Standing Technical Committee Strategic Plan Space Conditioning Standing Technical Committee Strategic Plan This strategic plan document outlines the gaps,...

  5. Total Space Heating Water Heating Cook-

    Gasoline and Diesel Fuel Update (EIA)

    Tables Total Space Heating Water Heating Cook- ing Other Total Space Heating Water Heating Cook- ing Other All Buildings ... 636 580 46 1 Q 114.0...

  6. Los Alamos Space Weather Summer School

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    Non-U.S Citizens Mentors, Projects Papers, Reports Photos NSEC IGPPS Space Weather Summer School Los Alamos Space Weather Summer School June 1 - July 24, 2015 Contacts...

  7. Integration of space weather into space situational awareness

    SciTech Connect (OSTI)

    Reeves, Geoffrey D

    2010-11-09

    Rapid assessment of space weather effects on satellites is a critical step in anomaly resolution and satellite threat assessment. That step, however, is often hindered by a number of factors including timely collection and delivery of space weather data and the inherent com plexity of space weather information. As part of a larger, integrated space situational awareness program, Los Alamos National Laboratory has developed prototype operational space weather tools that run in real time and present operators with customized, user-specific information. The Dynamic Radiation Environment Assimilation Model (DREAM) focuses on the penetrating radiation environment from natural or nuclear-produced radiation belts. The penetrating radiation environment is highly dynamic and highly orbit-dependent. Operators often must rely only on line plots of 2 MeV electron flux from the NOAA geosynchronous GOES satellites which is then assumed to be representative of the environment at the satellite of interest. DREAM uses data assimilation to produce a global, real-time, energy dependent specification. User tools are built around a distributed service oriented architecture (SOA) which will allow operators to select any satellite from the space catalog and examine the environment for that specific satellite and time of interest. Depending on the application operators may need to examine instantaneous dose rates and/or dose accumulated over various lengths of time. Further, different energy thresholds can be selected depending on the shielding on the satellite or instrument of interest. In order to rapidly assess the probability that space weather was the cause of anomalous operations, the current conditions can be compared against the historical distribution of radiation levels for that orbit. In the simplest operation a user would select a satellite and time of interest and immediately see if the environmental conditions were typical, elevated, or extreme based on how often those conditions occur in that orbit. This allows users to rapidly rule in or out environmental causes of anomalies. The same user interface can also allow users to drill down for more detailed quantitative information. DREAM can be run either from a distributed web-based user interface or as a stand-alone application for secure operations. In this paper we discuss the underlying structure of the DREAM model and demonstrate the user interface that we have developed . We also present some prototype data products and user interfaces for DREAM and discuss how space environment information can be seamlessly integrated into operational SSA systems.

  8. National Aeronautics and Space Administration Space Launch System

    E-Print Network [OSTI]

    Waliser, Duane E.

    engine. #12;The B-2 test stand at NASA's Stennis Space Center in Mississippi--originally built to test cryogenic liquid hydrogen and liquid oxygen that will feed the vehicle's RS-25 engines. SLS is an advanced, heavy-lift launch vehicle that will provide an entirely new capability for science and human exploration

  9. National Aeronautics and Space Administration space launch system

    E-Print Network [OSTI]

    Waliser, Duane E.

    Shuttle Main Engine Processing Facility, solid rocket motor test firing, J-2X test firing #12;Providing Heavy-Lift Launch Vehicle NASA's Space Launch System is an advanced, heavy-lift launch vehicle which including near-Earth asteroids, Lagrange points, the moon and ultimately Mars. The SLS heavy-lift launch

  10. Atmospheric,OceanicandSpaceSciences Atmospheric, Oceanic & Space Sciences

    E-Print Network [OSTI]

    Eustice, Ryan

    Research Areas High Energy Density Physics/Laboratory Astrophysics Magnetospheric & Ionosphere/Thermosphere Physics Planetary Magnetospheres Solar & Heliospheric Physics Space Weather Aeronomy For Faculty involved,Recipient, Department of Energy Early Career Award Margaret Kivelson, Member, National Academy of Sciences; Member

  11. Space-Based Gravity Detector for a Space Laboratory

    E-Print Network [OSTI]

    Leonid Verozub

    2009-04-13

    A space-based superconducting gravitational low-frequency wave detector is considered. Sensitivity of the detector is sufficient to use the detector as a partner of other contemporary low-frequency detectors like LIGO and LISA. This device can also be very useful for experimental study of other effects predicted by theories of gravitation.

  12. Contemporary Mathematics Time-space and Space-times

    E-Print Network [OSTI]

    Laudal, Arnfinn

    use some of the basic concepts and philosophy of classical physics in the study of the geometry parametrized by the moduli space is then formulated in much the same way as in modern physics. Contents: §0 is to apply some basic concepts of classical physics to the study of the geometry of some algebraic geometric

  13. National Aeronautics and Space Administration space launch system

    E-Print Network [OSTI]

    Rathbun, Julie A.

    into the solar system--developing new technologies, inspiring future generations and expanding our knowledge Launch System 70t vehicle launching from Kennedy Space Center. Building America's New Rocket for Deep in the solar system, launching crews of up to four astronauts aboard the new Orion spacecraft to explore

  14. Calibration of Time Of Flight Detectors Using Laser-driven Neutron Source

    E-Print Network [OSTI]

    S. R. Mirfayzi; S. Kar; H. Ahmed; A. G. Krygier; A. Green; A. Alejo; R. Clarke; R. R. Freeman; J. Fuchs; D. Jung; A. Kleinschmidt; J. T. Morrison; Z. Najmudin; H. Nakamura; P. Norreys; M. Oliver; M. Roth; L. Vassura; M. Zepf; M. Borghesi

    2015-06-15

    Calibration of three scintillators (EJ232Q, BC422Q and EJ410) in a time-of-flight (TOF) arrangement using a laser drive-neutron source is presented. The three plastic scintillator detectors were calibrated with gamma insensitive bubble detector spectrometers, which were absolutely calibrated over a wide range of neutron energies ranging from sub MeV to 20 MeV. A typical set of data obtained simultaneously by the detectors are shown, measuring the neutron spectrum emitted from a petawatt laser irradiated thin foil.

  15. Time-of-flight discrimination between gamma-rays and neutrons by neural networks

    E-Print Network [OSTI]

    Serkan Akkoyun

    2012-08-13

    In gamma-ray spectroscopy, a number of neutrons are emitted from the nuclei together with the gamma-rays and these neutrons influence gamma-ray spectra. An obvious method of separating between neutrons and gamma-rays is based on the time-of-flight (tof) technique. This work aims obtaining tof distributions of gamma-rays and neutrons by using feed-forward artificial neural network (ANN). It was shown that, ANN can correctly classify gamma-ray and neutron events. Testing of trained networks on experimental data clearly shows up tof discrimination of gamma-rays and neutrons.

  16. A silicon photomultiplier readout for time of flight neutron spectroscopy with {gamma}-ray detectors

    SciTech Connect (OSTI)

    Pietropaolo, A.; Gorini, G.; Festa, G.; Andreani, C.; De Pascale, M. P.; Reali, E.; Grazzi, F.; Schooneveld, E. M.

    2009-09-15

    The silicon photomultiplier (SiPM) is a recently developed photosensor used in particle physics, e.g., for detection of minimum ionizing particles and/or Cherenkov radiation. Its performance is comparable to that of photomultiplier tubes, but with advantages in terms of reduced volume and magnetic field insensitivity. In the present study, the performance of a gamma ray detector made of an yttrium aluminum perovskite scintillation crystal and a SiPM-based readout is assessed for use in time of flight neutron spectroscopy. Measurements performed at the ISIS pulsed neutron source demonstrate the feasibility of {gamma}-detection based on the new device.

  17. Testing a new NIF neutron time-of-flight detector with a bibenzyl scintillator on OMEGA

    SciTech Connect (OSTI)

    Glebov, V. Yu.; Forrest, C.; Knauer, J. P.; Pruyne, A.; Romanofsky, M.; Sangster, T. C.; Shoup, M. J. III; Stoeckl, C.; Caggiano, J. A.; Carman, M. L.; Clancy, T. J.; Hatarik, R.; McNaney, J.; Zaitseva, N. P.

    2012-10-15

    A new neutron time-of-flight (nTOF) detector with a bibenzyl crystal as a scintillator has been designed and manufactured for the National Ignition Facility (NIF). This detector will replace a nTOF20-Spec detector with an oxygenated xylene scintillator currently operational on the NIF to improve the areal-density measurements. In addition to areal density, the bibenzyl detector will measure the D-D and D-T neutron yield and the ion temperature of indirect- and direct-drive-implosion experiments. The design of the bibenzyl detector and results of tests on the OMEGA Laser System are presented.

  18. A radial collimator for a time-of-flight neutron spectrometer

    SciTech Connect (OSTI)

    Stone, M. B.; Abernathy, D. L. [Quantum Condensed Matter Science Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States); Niedziela, J. L.; Loguillo, M. J.; Overbay, M. A. [Instrument and Source Division, Oak Ridge National Laboratory, Oak Ridge, Tennessee 37831 (United States)

    2014-08-15

    We have engineered and installed a radial collimator for use in the scattered beam of a neutron time-of-flight spectrometer at a spallation neutron source. The radial collimator may be used with both thermal and epithermal neutrons, reducing the detected scattering intensity due to material outside of the sample region substantially. The collimator is located inside of the sample chamber of the instrument, which routinely cycles between atmospheric conditions and cryogenic vacuum. The oscillation and support mechanism of the collimator allow it to be removed from use without breaking vacuum. We describe here the design and characterization of this radial collimator.

  19. Quantum time-of-flight measurements: kick clock versus continuous clock

    E-Print Network [OSTI]

    D. Alonso; R. Sala Mayato; J. G. Muga

    2002-05-22

    The measurement of time durations or instants of ocurrence of events has been frequently modelled ``operationally'' by coupling the system of interest to a ``clock''. According to several of these models the operational approach is limited at low energies because the perturbation of the clock does not allow to reproduce accurately the corresponding ideal time quantity, defined for the system in isolation. We show that, for a time-of-flight measurement model that can be set to measure dwell or arrival times, these limitations may be overcome by extending the range of energies where the clock works properly using pulsed couplings rather than continuous ones.

  20. Solid Phase Microextraction and Miniature Time-of-Flight Mass Spectrometer

    SciTech Connect (OSTI)

    Hiller, j.m.

    1999-01-26

    A miniature mass spectrometer, based on the time-of-flight principle, has been developed for the detection of chemical warfare agent precursor molecules. The instrument, with minor modifications, could fulfill many of the needs for sensing organic molecules in various Defense Programs, including Enhanced Surveillance. The basic footprint of the instrument is about that of a lunch box. The instrument has a mass range to about 300, has parts-per-trillion detection limits, and can return spectra in less than a second. The instrument can also detect permanent gases and is especially sensitive to hydrogen. In volume, the device could be manufactured for under $5000.

  1. Identification of powered parafoil-vehicle dynamics from modelling and flight test data 

    E-Print Network [OSTI]

    Hur, Gi-Bong

    2006-08-16

    S consisting of N particles P1,...,PN, suppose that n -m gen- eralized speeds have been introduced, and let vPir denote the rth partial velocity of Pi. Then, if Ri is the resultant of all contact and body forces acting on Pi, then the n -m quantities F1,...,Fn-m...IDENTIFICATION OF POWERED PARAFOIL-VEHICLE DYNAMICS FROM MODELLING AND FLIGHT TEST DATA A Dissertation by GI-BONG HUR Submitted to the Office of Graduate Studies of Texas A&M University in partial fulfillment of the requirements for the degree...

  2. RIB in-flight production and the facility EXOTIC at LNL

    SciTech Connect (OSTI)

    Mazzocco, Marco [Dipartimento di Fisica e Astronomia, Universitŕ di Padova and INFN-Sezione di Padova, via F. Marzolo 8, I-35131 Padova (Italy)

    2014-05-09

    The production of Radioactive Ion Beams (RIBs) via the In-Flight technique is reviewed. This separation method typically employs four main production mechanisms: (i) Projectile Fragmentation; (ii) Projectile Fission; (iii) Nuclear Fusion and (iv) Direct Processes in Inverse Kinematics. We will concentrate particularly on the last mechanism, the one used by the facility EXOTIC at the INFN-Laboratori Nazionali di Legnaro (LNL) for the production of light RIBs. An extensive description of the facility and a brief overview of the most recent scientific achievements with {sup 7}Be and {sup 17}F are given.

  3. TIME-OF-FLIGHT MASS MEASUREMENTS AND THEIR IMPORTANCE FOR NUCLEAR ASTROPHYSICS

    SciTech Connect (OSTI)

    Matos, M.; Shapira, Dan

    2009-01-01

    Atomic masses play an important role in nuclear astrophysics. The lack of experimental values for nuclides of interest has triggered a rapid development of new mass measurement devices around the world, including Time-of-Flight (TOF) mass measurements offering an access to the most exotic nuclides. Recently, the TOF-B rho technique that includes a position measurement for magnetic rigidity correction has been implemented at the NSCL. An experiment with a similar TOF-B rho technique is approved and planned at the next generation radioactive beam facility (RIBF) at RIKEN.

  4. David Kortenkamp NASA Johnson Space Center

    E-Print Network [OSTI]

    Kortenkamp, David

    David Kortenkamp NASA Johnson Space Center David Kortenkamp NASA Johnson Space Center Distributed Systems David Kortenkamp NASA Johnson Space Center/Metrica Inc. Houston TX 77058 kortenkamp@jsc.nasa.gov http://www.traclabs.com/~korten David Kortenkamp NASA Johnson Space Center/Metrica Inc. Houston TX

  5. Searching for a parking space 

    E-Print Network [OSTI]

    Laurier, Eric

    2005-01-01

    If you drive a car, it’s a classic problem on the busy city streets, the search for a parking space. Merely driving in the inner city is a challenging and frustrating affair because it is full of one way streets, dead ...

  6. Prospects for space arms control

    SciTech Connect (OSTI)

    Pilat, J.F.

    1989-01-01

    At the recent Wyoming Ministerial, US Secretary of State Baker and Soviet Foreign Minister Shevardnadze signed a memorandum of understanding on a bilateral verification experiment and data exchange related to a prohibition on chemical weapons, an agreement on advance notification of certain strategic exercises, and an umbrella agreement on START trial verification and stability measures. Despite these substantive achievements in high priority areas for the United States and the Soviet Union, media attention on the ministerial focused on an offer by the Soviets that would allow a START agreement to be concluded without a resolution of US-Soviet differences in the Defense and Space (D S) talks. Of course, the Soviet offer did not delink'' START and D S, because the Soviets continued to demand the right to withdraw from START if the United States deployed space-based defenses. A more substantial proposal on Defense and Space was the US initiative inviting a group of Soviet experts to visit Los Alamos and the TRW Corporation's test facility in San Juan Capistrano to learn more about US SDI research activities. The US invitation was proposed in the context of the Predictability Measures Protocol to a Defense and Space Treaty, tabled by the United States, which calls for regular exchanges of data, briefings, visits to laboratories, and observation of tests designed to foster transparency and predictability.

  7. Upper Estimates for Banach Spaces 

    E-Print Network [OSTI]

    Freeman, Daniel B.

    2010-10-12

    We study the relationship of dominance for sequences and trees in Banach spaces. In the context of sequences, we prove that domination of weakly null sequences is a uniform property. More precisely, if $(v_i)$ is a normalized basic sequence and $X...

  8. National Aeronautics and Space Administration

    E-Print Network [OSTI]

    Rathbun, Julie A.

    -generation space fleet, Orion will push the envelope of human spaceflight far beyond low Earth orbit. Orion may features dozens of technology advancements and innovations that have been incorporated into the spacecraft and avionics systems. Building upon the best of Apollo and shuttle-era design, the Orion spacecraft includes

  9. Fusion for Earth and Space

    SciTech Connect (OSTI)

    Williams, Pharis E

    2009-03-16

    The compact reactor concept (Williams, 2007) has the potential to provide clean, safe and unlimited supply of energy for Earth and Space applications. The concept is a potential fusion reactor wherein deuterium nuclei are preferentially fused into helium nuclei. Because the deuterium nuclei are preferentially fused into helium nuclei at temperatures and energies lower than specified by the standard model there is no harmful radiation as a byproduct of this fusion process. Therefore, a reactor using this reaction does not need any shielding to contain such radiation. The energy released from each reaction and the absence of shielding makes the deuterium-plus-deuterium-to-helium (DDH) reactor very compact when compared to other reactors, both fission and fusion types. Moreover, the potential energy output per reactor weight and the absence of harmful radiation makes the DDH reactor an ideal candidate for individual home and space power. The concept also would make it possible for each plant or remote location to have it's own power source, on site, without the need for a connection to the power grid. This would minimize, or eliminate, power blackouts. The concept could replace large fission reactors and fossil fuel power plants plus provide energy for ships, locomotives, trucks and autos. It would make an ideal source of energy for space power applications and for space propulsion.

  10. Space Risks: A new generation

    E-Print Network [OSTI]

    Schrijver, Karel

    the capacity to travel and live in space, we can reach other planets and, most useful for our daily lives, we in orbit and ensuring the safety of installations on Earth. Insurers, therefore, are integral Our Specialists Contents 2 Executive summary 3 Introduction 4 Collision risks on the rise 12 Solar

  11. Magnetic fields on resistance spaces

    E-Print Network [OSTI]

    Michael Hinz; Luke Rogers

    2015-02-03

    On a metric measure space $X$ that supports a regular, strongly local resistance form we consider a magnetic energy form that corresponds to the magnetic Laplacian for a particle confined to $X$. We provide sufficient conditions for closability and self-adjointness in terms of geometric conditions on the reference measure without assuming energy dominance.

  12. Space

    Broader source: All U.S. Department of Energy (DOE) Office Webpages (Extended Search)

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Homesum_a_epg0_fpd_mmcf_m.xls" ,"Available from WebQuantity ofkandz-cm11 Outreach Home RoomPreservation ofAlbuquerque|SensitiveApril 2, 2014 Smith Named as NewApril

  13. Physical space and cosmology. I: Model

    E-Print Network [OSTI]

    Valeriy P. Polulyakh

    2011-02-01

    The nature of the physical space seems the most important subject in physics. A present paper proceeds from the assumption of physical reality of space contrary to the standard view of the space as a purely relational nonexistence - void. The space and its evolution are the primary sources of phenomena in Mega- and micro-worlds. Thus cosmology and particle physics have the same active agent - physical space.

  14. In-flight observations of low-mode ?R asymmetries in NIF implosions

    DOE Public Access Gateway for Energy & Science Beta (PAGES Beta)

    Zylstra, A. B. [Massachusetts Institute of Technology, Cambridge, MA (United States). Plasma Science and Fusion Center, High Energy Density Physics Div.; Frenje, J. A. [Plasma Science and Fusion Center, Massachusetts Institute of Technology, Cambridge, Massachusetts (United States)] (ORCID:0000000168460378); Seguin, F. H. [Massachusetts Institute of Technology, Cambridge, MA (United States). Plasma Science and Fusion Center, High Energy Density Physics Div.; Rygg, J. R. [Lawrence Livermore National Laboratory, Livermore, California (United States); Kritcher, A. [Lawrence Livermore National Laboratory, Livermore, California (United States); Rosenberg, M. J. [Plasma Science and Fusion Center, Massachusetts Institute of Technology, Cambridge, Massachusetts (United States); Rinderknecht, H. G. [Massachusetts Institute of Technology, Cambridge, MA (United States). Plasma Science and Fusion Center, High Energy Density Physics Div.; Hicks, D. G. [Lawrence Livermore National Laboratory, Livermore, California (United States)] (ORCID:0000000183229983); Friedrich, S. [Lawrence Livermore National Laboratory, Livermore, California (United States); Bionta, R. [Lawrence Livermore National Laboratory, Livermore, California (United States); Meezan, N. B. [Lawrence Livermore National Laboratory, Livermore, California (United States); Olson, R. [Los Alamos National Laboratory, Los Alamos, New Mexico (United States); Atherton, J. [Lawrence Livermore National Laboratory, Livermore, California (United States); Barrios, M. [Lawrence Livermore National Laboratory, Livermore, California (United States); Bell, P. [Lawrence Livermore National Laboratory, Livermore, California (United States); Benedetti, R. [Lawrence Livermore National Laboratory, Livermore, California (United States); Berzak Hopkins, L. [Lawrence Livermore National Laboratory, Livermore, California (United States)] (ORCID:0000000291875667); Betti, R. [Laboratory for Laser Energetics, University of Rochester, Rochester, New York (United States); Bradley, D. [Lawrence Livermore National Laboratory, Livermore, California (United States); Callahan, D. [Lawrence Livermore National Laboratory, Livermore, California (United States)] (ORCID:0000000315498916); Casey, D. [Lawrence Livermore National Laboratory, Livermore, California (United States); Collins, G. [Lawrence Livermore National Laboratory, Livermore, California (United States); Dewald, E. L. [Lawrence Livermore National Laboratory, Livermore, California (United States); Dixit, S. [Lawrence Livermore National Laboratory, Livermore, California (United States); Doppner, T. [Lawrence Livermore National Laboratory, Livermore, California (United States); Edwards, M. J. [Lawrence Livermore National Laboratory, Livermore, California (United States); Gatu Johnson, M. [Plasma Science and Fusion Center, Massachusetts Institute of Technology, Cambridge, Massachusetts (United States); Glenn, S. [Lawrence Livermore National Laboratory, Livermore, California (United States); Grim, G. [Los Alamos National Laboratory, Los Alamos, New Mexico (United States); Hatchett, S. [Lawrence Livermore National Laboratory,Livermore, California (United States); Jones, O. [Lawrence Livermore National Laboratory, Livermore, California (United States); Khan, S. [Lawrence Livermore National Laboratory, Livermore, California (United States); Kilkenny, J. [General Atomics, San Diego, California (United States); Kline, J. [Los Alamos National Laboratory, Los Alamos, New Mexico (United States); Knauer, J. [Laboratory for Laser Energetics, University of Rochester, Rochester, New York (United States); Kyrala, G. [Los Alamos National Laboratory, Los Alamos, New Mexico (United States)] (ORCID:0000000336850798); Landen, O. [Lawrence Livermore National Laboratory, Livermore, California (United States); LePape, S. [Lawrence Livermore National Laboratory, Livermore, California (United States); Li, C. K. [Plasma Science and Fusion Center, Massachusetts Institute of Technology, Cambridge, Massachusetts (United States); Lindl, J. [Lawrence Livermore National Laboratory, Livermore, California (United States)

    2015-05-01

    Charged-particle spectroscopy is used to assess implosion symmetry in ignition-scale indirect-drive implosions for the first time. Surrogate D3He gas-filled implosions at the National Ignition Facility produce energetic protons via D+3He fusion that are used to measure the implosion areal density (?R) at the shock-bang time. By using protons produced several hundred ps before the main compression bang, the implosion is diagnosed in-flight at a convergence ratio of 3-5 just prior to peak velocity. This isolates acceleration-phase asymmetry growth. For many surrogate implosions, proton spectrometers placed at the north pole and equator reveal significant asymmetries with amplitudes routinely ?10%, which are interpreted as l=2 Legendre modes. With significant expected growth by stagnation, it is likely that these asymmetries would degrade the final implosion performance. X-ray self-emission images at stagnation show asymmetries that are positively correlated with the observed in-flight asymmetries and comparable in magnitude, contradicting growth models; this suggests that the hot-spot shape does not reflect the stagnated shell shape or that significant residual kinetic energy exists at stagnation. More prolate implosions are observed when the laser drive is sustained (“no-coast”), implying a significant time-dependent asymmetry in peak drive.

  15. A Fast Pulsed Neutron Source for Time-of-Flight Detection of Nuclear Materials and Explosives

    SciTech Connect (OSTI)

    Krishnan, Mahadevan; Bures, Brian; James, Colt; Madden, Robert [Alameda Applied Sciences Corporation, 3077 Teagarden Street, San Leandro, CA 94577 (United States); Hennig, Wolfgang; Breus, Dimitry; Asztalos, Stephen; Sabourov, Konstantin [XIA LLC, 31057 Genstar Road, Hayward, CA 94544 (United States); Lane, Stephen [NSF Center for Biophotonics and School of Medicine, University of California Davis, Sacramento CA, 95817 (United States)

    2011-12-13

    AASC has built a fast pulsed neutron source based on the Dense Plasma Focus (DPF). The more current version stores only 100 J but fires at {approx}10-50 Hz and emits {approx}10{sup 6}n/pulse at a peak current of 100 kA. Both sources emit 2.45{+-}0.1 MeV(DD) neutron pulses of {approx}25-40 ns width. Such fast, quasi-monoenergetic pulses allow time-of-flight detection of characteristic emissions from nuclear materials or high explosives. A test is described in which iron targets were placed at different distances from the point neutron source. Detectors such as Stilbene and LaBr3 were used to capture inelastically induced, 847 keV gammas from the iron target. Shielding of the source and detectors eliminated most (but not all) of the source neutrons from the detectors. Gated detection, pulse shape analysis and time-of-flight discrimination enable separation of gamma and neutron signatures and localization of the target. A Monte Carlo simulation allows evaluation of the potential of such a fast pulsed source for a field-portable detection system. The high rep-rate source occupies two 200 liter drums and uses a cooled DPF Head that is <500 cm{sup 3} in volume.

  16. Lanthanum halide scintillators for time-of-flight 3-D pet

    DOE Patents [OSTI]

    Karp, Joel S. (Glenside, PA); Surti, Suleman (Philadelphia, PA)

    2008-06-03

    A Lanthanum Halide scintillator (for example LaCl.sub.3 and LaBr.sub.3) with fast decay time and good timing resolution, as well as high light output and good energy resolution, is used in the design of a PET scanner. The PET scanner includes a cavity for accepting a patient and a plurality of PET detector modules arranged in an approximately cylindrical configuration about the cavity. Each PET detector includes a Lanthanum Halide scintillator having a plurality of Lanthanum Halide crystals, a light guide, and a plurality of photomultiplier tubes arranged respectively peripherally around the cavity. The good timing resolution enables a time-of-flight (TOF) PET scanner to be developed that exhibits a reduction in noise propagation during image reconstruction and a gain in the signal-to-noise ratio. Such a PET scanner includes a time stamp circuit that records the time of receipt of gamma rays by respective PET detectors and provides timing data outputs that are provided to a processor that, in turn, calculates time-of-flight (TOF) of gamma rays through a patient in the cavity and uses the TOF of gamma rays in the reconstruction of images of the patient.

  17. In-flight observations of low-mode ?R asymmetries in NIF implosions

    DOE Public Access Gateway for Energy & Science Beta (PAGES Beta)

    Zylstra, A. B.; Frenje, J. A.; Seguin, F. H.; Rygg, J. R.; Kritcher, A.; Rosenberg, M. J.; Rinderknecht, H. G.; Hicks, D. G.; Friedrich, S.; Bionta, R.; et al

    2015-05-01

    Charged-particle spectroscopy is used to assess implosion symmetry in ignition-scale indirect-drive implosions for the first time. Surrogate D3He gas-filled implosions at the National Ignition Facility produce energetic protons via D+3He fusion that are used to measure the implosion areal density (?R) at the shock-bang time. By using protons produced several hundred ps before the main compression bang, the implosion is diagnosed in-flight at a convergence ratio of 3-5 just prior to peak velocity. This isolates acceleration-phase asymmetry growth. For many surrogate implosions, proton spectrometers placed at the north pole and equator reveal significant asymmetries with amplitudes routinely ?10%, which aremore »interpreted as l=2 Legendre modes. With significant expected growth by stagnation, it is likely that these asymmetries would degrade the final implosion performance. X-ray self-emission images at stagnation show asymmetries that are positively correlated with the observed in-flight asymmetries and comparable in magnitude, contradicting growth models; this suggests that the hot-spot shape does not reflect the stagnated shell shape or that significant residual kinetic energy exists at stagnation. More prolate implosions are observed when the laser drive is sustained (“no-coast”), implying a significant time-dependent asymmetry in peak drive.« less

  18. CAPITAL PLANNING AND SPACE MANAGEMENT GUIDELINES FOR THE USE OF OUTDOOR SPACE ON THE CAMPUS OF

    E-Print Network [OSTI]

    CAPITAL PLANNING AND SPACE MANAGEMENT GUIDELINES FOR THE USE OF OUTDOOR SPACE ON THE CAMPUS SPACE AND OUTDOOR SPACE Capital Planning and Space Management offers event scheduling to student taking responsibility and agreeing to reimburse the University for the Cost of whatever damage

  19. United Nations Human Space Technology Initiative (HSTI)

    E-Print Network [OSTI]

    Ochiai, M; Steffens, H; Balogh, W; Haubold, H J; Othman, M; Doi, T

    2015-01-01

    The Human Space Technology Initiative was launched in 2010 within the framework of the United Nations Programme on Space Applications implemented by the Office for Outer Space Affairs of the United Nations. It aims to involve more countries in activities related to human spaceflight and space exploration and to increase the benefits from the outcome of such activities through international cooperation, to make space exploration a truly international effort. The role of the Initiative in these efforts is to provide a platform to exchange information, foster collaboration between partners from spacefaring and non-spacefaring countries, and encourage emerging and developing countries to take part in space research and benefit from space applications. The Initiative organizes expert meetings and workshops annually to raise awareness of the current status of space exploration activities as well as of the benefits of utilizing human space technology and its applications. The Initiative is also carrying out primary ...

  20. Large aperture diffractive space telescope

    DOE Patents [OSTI]

    Hyde, Roderick A. (Livermore, CA)

    2001-01-01

    A large (10's of meters) aperture space telescope including two separate spacecraft--an optical primary objective lens functioning as a magnifying glass and an optical secondary functioning as an eyepiece. The spacecraft are spaced up to several kilometers apart with the eyepiece directly behind the magnifying glass "aiming" at an intended target with their relative orientation determining the optical axis of the telescope and hence the targets being observed. The objective lens includes a very large-aperture, very-thin-membrane, diffractive lens, e.g., a Fresnel lens, which intercepts incoming light over its full aperture and focuses it towards the eyepiece. The eyepiece has a much smaller, meter-scale aperture and is designed to move along the focal surface of the objective lens, gathering up the incoming light and converting it to high quality images. The positions of the two space craft are controlled both to maintain a good optical focus and to point at desired targets which may be either earth bound or celestial.

  1. Reduced pressure and temperature reclamation of water using the GE Integrated Water-waste Management System for potential space flight application 

    E-Print Network [OSTI]

    Chowdhury, Hasan Imtiaz

    1989-01-01

    hardware and verify the results previously reported by GE, the following series of tests were performed: 1) Disassemble, clean, and reassemble the system. 2) Determine the condensation rate as a function of temperature of the evaporator and the condenser... derivative (PID) feedback control sensor. The cooling system devised has a capacity of 1465 W and is controlled by an on/otf temperature sensor operating through a time delay relay. B. RESULTS AND DISCUSSION The system characterization procedure consisted...

  2. NASA's Marshall Space Flight Center Improves Cooling System Performance: Best Management Practice Case Study #10: Cooling Towers (Revised) (Fact Sheet), Federal Energy Management Program (FEMP)

    Energy Savers [EERE]

    AFDC Printable Version Share this resource Send a link to EERE: Alternative Fuels Data Center Home Page to someone by E-mail Share EERE: Alternative Fuels Data Center Home Page on Facebook Tweet about EERE: Alternative Fuels Data Center Home Page on Twitter Bookmark EERE: Alternative Fuels Data Center Home Page on Google Bookmark EERE: Alternative Fuels Data Center Home Page on DeliciousMathematicsEnergyInterested Parties -Department of EnergyNEW YORK STATENASA Enhanced Use Lease

  3. Relativity theory in time-space

    E-Print Network [OSTI]

    Ákos G. Horváth

    2014-11-05

    The concept of time-space defined in an earlier paper of the author is certain generalization of the so-called space-time. In this paper we introduce the concept of time-space manifold. In the homogeneous case, the time-space manifold is a differentiable manifold with such tangent spaces which have certain fixed time-space structure. We redefine the fundamental concepts of global relativity theory with respect to this general situation. We study the concepts of affine connection, parallel transport, curvature tensor and Einstein equation, respectively.

  4. A performance-driven experiment framework for space technology development using the International Space Station

    E-Print Network [OSTI]

    Hilton, Andrew Robert

    2015-01-01

    Space systems are inherently difficult to verify prior to launch due to the challenges of replicating the space environment through ground testing. The SPHERES testbed on the International Space Station has provided a ...

  5. Space and motion : data based rules of public space pedestrian motion

    E-Print Network [OSTI]

    Gonzalez Rojas, Paloma (Paloma Francisca)

    2015-01-01

    The understanding of space relies on motion, as we experience space by crossing it. While in motion we sense the environment in time, interacting with space. The vision of this thesis is to incorporate people's motion into ...

  6. A computational approach for hypersonic nonequilibrium radiation utilizing space partition algorithm and Gauss quadrature

    SciTech Connect (OSTI)

    Shang, J.S. [Wright State University, Dayton, OH (United States); Andrienko, D.A. [Wright State University, Dayton, OH (United States); Institute for Problems in Mechanics, Moscow, 119526 (Russian Federation); Huang, P.G. [Wright State University, Dayton, OH (United States); Surzhikov, S.T. [Institute for Problems in Mechanics, Moscow, 119526 (Russian Federation)

    2014-06-01

    An efficient computational capability for nonequilibrium radiation simulation via the ray tracing technique has been accomplished. The radiative rate equation is iteratively coupled with the aerodynamic conservation laws including nonequilibrium chemical and chemical–physical kinetic models. The spectral properties along tracing rays are determined by a space partition algorithm of the nearest neighbor search process, and the numerical accuracy is further enhanced by a local resolution refinement using the Gauss–Lobatto polynomial. The interdisciplinary governing equations are solved by an implicit delta formulation through the diminishing residual approach. The axisymmetric radiating flow fields over the reentry RAM-CII probe have been simulated and verified with flight data and previous solutions by traditional methods. A computational efficiency gain nearly forty times is realized over that of the existing simulation procedures.

  7. Flags in Space: NASA Symbols and Flags in the U.S. Manned Space Program

    E-Print Network [OSTI]

    Platoff, Anne M.

    sory Committee for Aeronautics. 4. NASA Policy Directive (When the National Aeronautics and Space Administra- tion (passed the National Aeronautics and Space Act and it was

  8. Technical bases to consider for performance and demonstration testing of space fission reactors

    SciTech Connect (OSTI)

    Hixson, L. L. (Laurie L.); Houts, M. G. (Michael G.); Clement, S. D. (Steven D.)

    2004-01-01

    Performance and demonstration testing are critical to the success of a space fission reactor program. However, the type and extent to which testing of space reactors should be performed has been a point of discussion within the industry for many years. With regard to full power ground nuclear tests, questions such as: (1) Do the benefits outweigh the risks; (2) Are there equivalent alternatives; (3) Can a test facility be constructed (or modified) in a reasonable amount of time; (4) Will the test article accurately represent the flight system; and (5) Are the costs too restrictive, have been debated for decades. There are obvious benefits of full power ground nuclear testing such as obtaining systems integrated reliability data on a full-scale, complete end-to-end system. But these benefits come at some programmatic risk. In addition, this type of testing does not address safety related issues. This paper will discuss and assess these and other technical considerations essential in deciding which type of performance and demonstration testing to conduct on space fission reactor systems.

  9. Embeddings and factorizations of Banach spaces 

    E-Print Network [OSTI]

    Zheng, Bentuo

    2009-05-15

    One problem, considered important in Banach space theory since at least the 1970’s, asks for intrinsic characterizations of subspaces of a Banach space with an unconditional basis. A more general question is to give necessary and sufficient...

  10. Space applications of shape memory alloys 

    E-Print Network [OSTI]

    Godard, Olivier Jean

    2002-01-01

    This work presents an investigation of two new possible space applications of shape memory alloys. The first application uses these alloys as active devices to optimally reorient solar panels in space. The thermal issues related to the actuation...

  11. Space Weather Prediction with Exascale Computing

    E-Print Network [OSTI]

    Lapenta, Giovanni

    2011-01-01

    Space weather refers to conditions on the Sun, in the interplanetary space and in the Earth space environment that can influence the performance and reliability of space-borne and ground-based technological systems and can endanger human life or health. Adverse conditions in the space environment can cause disruption of satellite operations, communications, navigation, and electric power distribution grids, leading to a variety of socioeconomic losses. The conditions in space are also linked to the Earth climate. The activity of the Sun affects the total amount of heat and light reaching the Earth and the amount of cosmic rays arriving in the atmosphere, a phenomenon linked with the amount of cloud cover and precipitation. Given these great impacts on society, space weather is attracting a growing attention and is the subject of international efforts worldwide. We focus here on the steps necessary for achieving a true physics-based ability to predict the arrival and consequences of major space weather storms....

  12. NASA Creates Space Technology Mission Directorate

    E-Print Network [OSTI]

    drew media attention and articles on 3D printing, including coverage by Popular Mechanics and website on 3D printing and prototyping technology to create parts for the Space Launch System at Marshall Space

  13. Ames Lab 101: Growing Crystals in Space

    SciTech Connect (OSTI)

    Trivedi, Rohit

    2011-01-01

    Rohit Trivedi, distinguished professor of materials science and engineering, discusses his research with NASA to grow crystals in space.

  14. Ames Lab 101: Growing Crystals in Space

    ScienceCinema (OSTI)

    Trivedi, Rohit

    2012-08-29

    Rohit Trivedi, distinguished professor of materials science and engineering, discusses his research with NASA to grow crystals in space.

  15. Alpha-muon sticking and chaos in muon-catalysed "in flight" d-t fusion

    E-Print Network [OSTI]

    Sachie Kimura; Aldo Bonasera

    2006-07-31

    We discuss the alpha-muon sticking coefficient in the muon-catalysed ``in flight" d-t fusion in the framework of the Constrained Molecular Dynamics model. Especially the influence of muonic chaotic dynamics on the sticking coefficient is brought into focus. The chaotic motion of the muon affects not only the fusion cross section but also the $\\mu-\\alpha$ sticking coefficient. Chaotic systems lead to larger enhancements with respect to regular systems because of the reduction of the tunneling region. Moreover they give smaller sticking probabilities than those of regular events. By utilizing a characteristic of the chaotic dynamics one can avoid losing the muon in the $\\mu$CF cycle. We propose the application of the so-called ``microwave ionization of a Rydberg atom" to the present case which could lead to the enhancement of the reactivation process by using X-rays.

  16. A new neutron time-of-flight detector for fuel-areal-density measurements on OMEGA

    SciTech Connect (OSTI)

    Glebov, V. Yu. Forrest, C. J.; Marshall, K. L.; Romanofsky, M.; Sangster, T. C.; Shoup, M. J.; Stoeckl, C.

    2014-11-15

    A new neutron time-of-flight (nTOF) detector for fuel-areal-density measurements in cryogenic DT implosions was installed on the OMEGA Laser System. The nTOF detector has a cylindrical thin-wall, stainless-steel, 8-in.-diam, 4-in.-thick cavity filled with an oxygenated liquid xylene scintillator. Four gated photomultiplier tubes (PMTs) with different gains are used to measure primary DT and D{sub 2} neutrons, down-scattered neutrons in nT and nD kinematic edge regions, and to study tertiary neutrons in the same detector. The nTOF detector is located 13.4 m from target chamber center in a well-collimated line of sight. The design details of the nTOF detector, PMT optimization, and test results on OMEGA will be presented.

  17. In-flight calibration of STEREO-B/WAVES antenna system

    E-Print Network [OSTI]

    Panchenko, M; Rucker, H O; Fischer, G; Oswald, T H; Cecconi, B; Maksimovic, M

    2015-01-01

    The STEREO/WAVES (SWAVES) experiment on board the two STEREO spacecraft (Solar Terrestrial Relations Observatory) launched on 25 October 2006 is dedicated to the measurement of the radio spectrum at frequencies between a few kilohertz and 16 MHz. The SWAVES antenna system consists of 6 m long orthogonal monopoles designed to measure the electric component of the radio waves. With this configuration direction finding of radio sources and polarimetry (analysis of the polarization state) of incident radio waves is possible. For the evaluation of the SWAVES data the receiving properties of the antennas, distorted by the radiation coupling with the spacecraft body and other onboard devices, have to be known accurately. In the present context, these properties are described by the antenna effective length vectors. We present the results of an in-flight calibration of the SWAVES antennas using the observations of the nonthermal terrestrial auroral kilometric radiation (AKR) during STEREO roll maneuvers in an early s...

  18. An implantable instrument for studying the long-term flight biology of migratory birds

    SciTech Connect (OSTI)

    Spivey, Robin J. E-mail: c.bishop@bangor.ac.uk; Bishop, Charles M. E-mail: c.bishop@bangor.ac.uk

    2014-01-15

    The design of an instrument deployed in a project studying the high altitude Himalayan migrations of bar-headed geese (Anser indicus) is described. The electronics of this archival datalogger measured 22 × 14 × 6.5 mm, weighed 3 g, was powered by a ˝AA-sized battery weighing 10 g and housed in a transparent biocompatible tube sealed with titanium electrodes for electrocardiography (ECG). The combined weight of 32 g represented less than 2% of the typical bodyweight of the geese. The primary tasks of the instrument were to continuously record a digitised ECG signal for heart-rate determination and store 12-bit triaxial accelerations sampled at 100 Hz with 15% coverage over each 2 min period. Measurement of atmospheric pressure provided an indication of altitude and rate of ascent or descent during flight. Geomagnetic field readings allowed for latitude estimation. These parameters were logged twice per minute along with body temperature. Data were stored to a memory card of 8 GB capacity. Instruments were implanted in geese captured on Mongolian lakes during the breeding season when the birds are temporarily flightless due to moulting. The goal was to collect data over a ten month period, covering both southward and northward migrations. This imposed extreme constraints on the design's power consumption. Raw ECG can be post-processed to obtain heart-rate, allowing improved rejection of signal interference due to strenuous activity of locomotory muscles during flight. Accelerometry can be used to monitor wing-beat frequency and body kinematics, and since the geese continued to flap their wings continuously even during rather steep descents, act as a proxy for biomechanical power. The instrument enables detailed investigation of the challenges faced by the geese during these arduous migrations which typically involve flying at extreme altitudes through cold, low density air where oxygen availability is significantly reduced compared to sea level.

  19. Ongoing Space Physics - Astrophysics Connections

    E-Print Network [OSTI]

    David Eichler

    2005-03-16

    I review several ongoing connections between space physics and astrophysics: a) Measurements of energetic particle spectra have confirmed theoretical prediction of the highest energy to which shocks can accelerate particles, and this has direct bearing on the origin of the highest energy cosmic rays. b) Mass ejection in solar flares may help us understand photon ejection in the giant flares of magnetar outbursts. c) Measurements of electron heat fluxes in the solar wind can help us understand whether heat flux in tenuous astrophysical plasma is in accordance with the classical Spitzer-Harm formula or whether it is reduced well below this value by plasma instabilities.

  20. Fractional Inversion in Krylov Space

    E-Print Network [OSTI]

    B. Bunk

    1998-05-28

    The fractional inverse $M^{-\\gamma}$ (real $\\gamma >0$) of a matrix $M$ is expanded in a series of Gegenbauer polynomials. If the spectrum of $M$ is confined to an ellipse not including the origin, convergence is exponential, with the same rate as for Chebyshev inversion. The approximants can be improved recursively and lead to an iterative solver for $M^\\gamma x = b$ in Krylov space. In case of $\\gamma = 1/2$, the expansion is in terms of Legendre polynomials, and rigorous bounds for the truncation error are derived.