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Hyperthermal Environments Simulator for Nuclear Rocket Engine DevelopmentAn arc-heater driven hyperthermal convective environments simulator was recently developed and commissioned for long duration hot hydrogen exposure of nuclear thermal rocket materials. This newly established non-nuclear testing capability uses a high-power, multi-gas, wall-stabilized constricted arc-heater to produce hightemperature pressurized hydrogen flows representative of nuclear reactor core environments, excepting radiation effects, and is intended to serve as a low-cost facility for supporting non-nuclear developmental testing of hightemperature fissile fuels and structural materials. The resulting reactor environments simulator represents a valuable addition to the available inventory of non-nuclear test facilities and is uniquely capable of investigating and characterizing candidate fuel/structural materials, improving associated processing/fabrication techniques, and simulating reactor thermal hydraulics. This paper summarizes facility design and engineering development efforts and reports baseline operational characteristics as determined from a series of performance mapping and long duration capability demonstration tests. Potential follow-on developmental strategies are also suggested in view of the technical and policy challenges ahead. Keywords: Nuclear Rocket Engine, Reactor Environments, Non-Nuclear Testing, Fissile Fuel Development.
Document ID
20110008816
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Litchford, Ron J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Foote, John P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Clifton, W. B.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hickman, Robert R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Wang, Ten-See
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Dobson, Christopher C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
February 7, 2011
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M11-0110
Report Number: M11-0110
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space 2011
Location: Albuquerque, NM
Country: United States
Start Date: February 7, 2011
End Date: February 10, 2011
Distribution Limits
Public
Copyright
Public Use Permitted.
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