Physics
Scientific paper
Nov 1979
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1979vina.nasa...30f&link_type=abstract
In its Viking Navigation p 30-47 (SEE N80-21397 12-15)
Physics
Earth-Mars Trajectories, Interplanetary Navigation, Viking 1 Spacecraft, Viking 2 Spacecraft, Orbit Calculation, Orbital Elements, Spacecraft Orbits, Trajectory Control
Scientific paper
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.
Dicken L. H.
Diehl Roger E.
Farless D. L.
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