The 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.
Trajectory description
1979-11-15
Miscellaneous
No indication
English
NTRS | 1973
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|Cassini Trajectory Design Description
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