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RCS propulsion functional path analysis for performance monitoring fault detection and annunciationThe operational flight instrumentation required for performance monitoring and fault detection are presented. Measurements by the burn through monitors are presented along with manifold and helium source pressures.
Document ID
19740026133
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Keesler, E. L. (Lockheed Electronics Co. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-140258
JSC-09130
LEC-3594
Accession Number
74N34246
Funding Number(s)
CONTRACT_GRANT: NAS9-12200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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