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Maneuver analysisThe maneuver analysis for the Mariner 9 mission, both prelaunch and in-flight, was different from that of previous Mariners because of the requirement to insert the spacecraft into orbit about Mars and to trim the orbit to an unprecedented accuracy. The most apparent differences were in the spacecraft design, the software development, and the maneuver strategy required for each phase of the mission. The analysis that was performed and the software that was developed, with emphasis on the maneuver strategy and actual in-flight results are described.
Document ID
19740021011
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mitchell, R. T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hintz, G. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Preston, G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 7, 2013
Publication Date
November 13, 1973
Publication Information
Publication: Its Mariner 9 Navigation
Subject Category
Navigation
Accession Number
74N29124
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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