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Title: NCSP IE and T&E Activities at Sandia.


Abstract not provided.

Publication Date:
Research Org.:
Sandia National Lab. (SNL-NM), Albuquerque, NM (United States)
Sponsoring Org.:
USDOE National Nuclear Security Administration (NNSA)
OSTI Identifier:
Report Number(s):
DOE Contract Number:
Resource Type:
Resource Relation:
Conference: Proposed for presentation at the NCSP Technical Program Revies held March 14-15, 2017 in Washington, DC.
Country of Publication:
United States

Citation Formats

Harms, Gary A. NCSP IE and T&E Activities at Sandia.. United States: N. p., 2017. Web.
Harms, Gary A. NCSP IE and T&E Activities at Sandia.. United States.
Harms, Gary A. Wed . "NCSP IE and T&E Activities at Sandia.". United States. doi:.
title = {NCSP IE and T&E Activities at Sandia.},
author = {Harms, Gary A.},
abstractNote = {Abstract not provided.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Wed Mar 01 00:00:00 EST 2017},
month = {Wed Mar 01 00:00:00 EST 2017}

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  • In a brief note like this, it will not be possible to survey all the many interesting and ingenious theoretical ideas that have been put forward to explain the e/sup +/e/sup -/ peaks observed at GSI. Rather, I should like to take this opportunity to make a few simple points. (AIP)
  • Simulation of hypersonic flight in ground test and evaluation (T and E) facilities is a challenging and formidable task, especially to fully duplicate the flight environment above approximately Mach 8 for most all hypersonic flight systems that have been developed, conceived, or envisioned. Basically, and for many years, the enabling technology to build such a ground test wind tunnel facility has been severely limited in the area of high-temperature, high-strength materials and thermal protection approaches. To circumvent the problems, various approaches have been used, including partial simulation and use of similarity laws and reduced test time. These approaches often aremore » not satisfactory, i.e. operability and durability testing for air-breathing propulsion development and thermal protection development of many flight systems. Thus, there is a strong need for science and technology (S and T) community involvement in technology development to address these problems. This paper discusses a specific case where this need exists and where significant S and T involvement has made and continues to make significant contributions. The case discussed will be an Air Force research program currently underway to develop enabling technologies for a Mach 8-15 hypersonic true temperature wind tunnel with relatively long run time. The research is based on a concept proposed by princeton University using radiant or beamed energy into the supersonic nozzle flow.« less