NASA NTRS · 19800012914
Trajectory description
Abstract
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.
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Farless, D. L., Dicken, L. H., Diehl, R. E.. 1979-11-15. Trajectory description. https://ntrs.nasa.gov/citations/19800012914
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