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Redesign of the Apollo cryogenic storage systemAn assessment of the Apollo 13 mission resulted in establishing new and revised requirements for the design of the oxygen tanks and the associated spacecraft system. Areas discussed include new system requirements, system changes to Apollo 14, revised operational requirements, instrumentation, operational redlines, component isolation modes, and return enhancement capabilities. In order to show the relationship of the cryogenic system to the spacecraft, a short description of the system is presented.
Document ID
19720016136
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bouman, C. P. (North American Rockwell Corp. Downey, CA, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1971
Publication Information
Publication: NASA. Manned Spacecraft Center MSCCryog. Symp. Papers
Subject Category
Propellants
Accession Number
72N23786
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19720016135Collected WorksMSC Cryogenics Symposium papers
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