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Title: Space vehicle electromechanical system and helical antenna winding fixture

Abstract

A space vehicle electromechanical system may employ an architecture that enables convenient and practical testing, reset, and retesting of solar panel and antenna deployment on the ground. A helical antenna winding fixture may facilitate winding and binding of the helical antenna.

Inventors:
; ; ; ; ; ;
Issue Date:
Research Org.:
Los Alamos National Laboratory (LANL), Los Alamos, NM (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1414918
Patent Number(s):
9853353
Application Number:
14/745,763
Assignee:
Los Alamos National Security, LLC (Los Alamos, NM)
Patent Classifications (CPCs):
B - PERFORMING OPERATIONS B64 - AIRCRAFT B64G - COSMONAUTICS
H - ELECTRICITY H01 - BASIC ELECTRIC ELEMENTS H01Q - ANTENNAS, i.e. RADIO AERIALS
DOE Contract Number:  
AC52-06NA25396
Resource Type:
Patent
Resource Relation:
Patent File Date: 2015 Jun 22
Country of Publication:
United States
Language:
English
Subject:
33 ADVANCED PROPULSION SYSTEMS; 42 ENGINEERING

Citation Formats

Judd, Stephen, Dallmann, Nicholas, Guenther, David, Enemark, Donald, Seitz, Daniel, Martinez, John, and Storms, Steven. Space vehicle electromechanical system and helical antenna winding fixture. United States: N. p., 2017. Web.
Judd, Stephen, Dallmann, Nicholas, Guenther, David, Enemark, Donald, Seitz, Daniel, Martinez, John, & Storms, Steven. Space vehicle electromechanical system and helical antenna winding fixture. United States.
Judd, Stephen, Dallmann, Nicholas, Guenther, David, Enemark, Donald, Seitz, Daniel, Martinez, John, and Storms, Steven. Tue . "Space vehicle electromechanical system and helical antenna winding fixture". United States. https://www.osti.gov/servlets/purl/1414918.
@article{osti_1414918,
title = {Space vehicle electromechanical system and helical antenna winding fixture},
author = {Judd, Stephen and Dallmann, Nicholas and Guenther, David and Enemark, Donald and Seitz, Daniel and Martinez, John and Storms, Steven},
abstractNote = {A space vehicle electromechanical system may employ an architecture that enables convenient and practical testing, reset, and retesting of solar panel and antenna deployment on the ground. A helical antenna winding fixture may facilitate winding and binding of the helical antenna.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2017},
month = {12}
}

Works referenced in this record:

Antenna erection mechanism
patent, October 1975


Portable collapsing antenna
patent, October 1984


Collapsible bifilar helical antenna
patent, October 1988


Payload adapter ring
patent, August 1991


Modular mother satellite bus for subsidiary payloads
patent, October 1992


Spacecraft antenna array with directivity enhancing rings
patent, February 1999


Multi-band concentric helical antenna
patent, November 1999


Dual polarized multifilar antenna
patent, October 2010


Self-deploying helical antenna
patent, May 2014


Deployable helical antenna for nano-satellites
patent, March 2015


Solar array transfer orbit power maximizer
patent, June 2015


Floating interface linkage
patent-application, April 2006


System For Simultaneous Tabbing And Stringing Of Solar Cells
patent-application, February 2010


Method for Connecting Solar Cells
patent-application, June 2012


Multi-Mode, Multi-Band Antenna
patent-application, September 2014