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Orbiter subsystem hardware/software interaction analysis. Volume 8: Forward reaction control systemThe results of the orbiter hardware/software interaction analysis for the AFT reaction control system are presented. The interaction between hardware failure modes and software are examined in order to identify associated issues and risks. All orbiter subsystems and interfacing program elements which interact with the orbiter computer flight software are analyzed. The failure modes identified in the subsystem/element failure mode and effects analysis are discussed.
Document ID
19800009823
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Becker, D. D. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Space Transportation
Report/Patent Number
JSC-14651-VOL-8
NASA-TM-80959
Report Number: JSC-14651-VOL-8
Report Number: NASA-TM-80959
Accession Number
80N18088
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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