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Mariner Mars 1971 attitude control subsystem flight performanceThe flight performance of the Mariner 71 attitude control subsystem is discussed. Each phase of the mission is delineated and the attitude control subsystem is evaluated within the observed operational environment. Performance anomalies are introduced and discussed within the context of general performance. Problems such as the sun sensor interface incompatibility, gas valve leaks, and scan platform dynamic coupling effects are given analytical considerations.
Document ID
19730013108
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schumacher, L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 15, 1973
Subject Category
Space Vehicles
Report/Patent Number
JPL-TM-33-600
NASA-CR-131522
Report Number: JPL-TM-33-600
Report Number: NASA-CR-131522
Accession Number
73N21835
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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