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Trajectory descriptionThe launch, interplanetary, encounter, and Mars orbit phases of the Viking 1 and 2 spacecraft trajectories are described. Time history plots of several parameters relative to the trajectories are presented along with tables of the geocentric, heliocentric, aerocentric, and injection orbital elements appropriate to each of the spacecraft trajectories.
Document ID
19800012914
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Farless, D. L. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Dicken, L. H. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Diehl, R. E. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 10, 2013
Publication Date
November 15, 1979
Publication Information
Publication: Viking Navigation
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
80N21399
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19800012912Collected WorksViking navigation
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