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A Hydrogen Containment Process for Nuclear Thermal Engine Ground testingThe objective of this study is to propose a new total hydrogen containment process to enable the testing required for NTP engine development. This H2 removal process comprises of two unit operations: an oxygen-rich burner and a shell-and-tube type of heat exchanger. This new process is demonstrated by simulation of the steady state operation of the engine firing at nominal conditions.
Document ID
20160009700
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Wang, Ten-See (NASA Marshall Space Flight Center Huntsville, AL, United States)
Stewart, Eric (NASA Marshall Space Flight Center Huntsville, AL, United States)
Canabal, Francisco (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 1, 2016
Publication Date
July 25, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Space Communications, Spacecraft Communications, Command And Tracking
Spacecraft Propulsion And Power
Report/Patent Number
M16-5403
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 25, 2016
End Date: July 27, 2016
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Engineering Education, Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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