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Reliability analysis of the Centaur IGS FIRST gimbal stabilization loopReliability analysis of Centaur inertial guidance system first gimbal stabilization loop
Document ID
19670016738
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Connor, W. S. (Research Triangle Inst. Durham, NC, United States)
Thompson, W. S. (Research Triangle Inst. Durham, NC, United States)
Date Acquired
August 3, 2013
Publication Date
December 2, 1963
Subject Category
Navigation
Report/Patent Number
NASA-CR-83962
GU-68
Report Number: NASA-CR-83962
Report Number: GU-68
Accession Number
67N26067
Funding Number(s)
CONTRACT_GRANT: NASW-334
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GIMBALLED CONTROL
CENTAUR LAUNCH VEHICLE
MATHEMATICAL MODEL
INERTIAL GUIDANCE
COMPONENT RELIABILITY

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