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Mars transit vehicle thermal protection system: Issues, options, and tradesA Mars mission is characterized by different mission phases. The thermal control of cryogenic propellant in a propulsive vehicle must withstand the different mission environments. Long term cryogenic storage may be achieved by passive or active systems. Passive cryo boiloff management features will include multilayer insulation, vapor cooled shield, and low conductance structural supports and penetrations. Active boiloff management incorporates the use of a refrigeration system. Key system trade areas include active verses passive system boiloff management (with respect to safety, reliability, and cost) and propellant tank insulation optimizations. Technology requirements include refrigeration technology advancements, insulation performance during long exposure, and cryogenic fluid transfer system for mission vehicle propellant tanking during vehicle buildip in LEO.
Document ID
19870008351
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brown, Norman
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1986
Publication Information
Publication: Manned Mars Mission. Working Group Papers, V. 2, Sect. 5, App.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N17784
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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