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Cryogenic Fluid Management Technology Development for Nuclear Thermal PropulsionCryogenic fluid management technology is critical to the success of future nuclear thermal propulsion powered vehicles and long duration missions. This paper discusses current capabilities in key technologies and their development path. The thermal environment, complicated from the radiation escaping a reactor of a nuclear thermal propulsion system, is examined and analysis presented. The technology development path required for maintaining cryogenic propellants in this environment is reviewed. This paper is intended to encourage and bring attention to the cryogenic fluid management technologies needed to enable nuclear thermal propulsion powered deep space missions.
Document ID
20150016543
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Taylor, B. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Caffrey, J.
(Oregon State Univ. Corvallis, OR, United States)
Hedayat, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Stephens, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Polsgrove, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 27, 2015
Publication Date
July 27, 2015
Subject Category
Propellants And Fuels
Spacecraft Propulsion And Power
Report/Patent Number
M15-4739
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference (AIAA Propulsion and Energy Forum 2015)
Location: Orlando, FL
Country: United States
Start Date: July 27, 2015
End Date: July 29, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society for Engineering Education (ASEE)
Distribution Limits
Public
Copyright
Public Use Permitted.
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