Orbit design and perturbation analysis for Mars rover and sample return mission concepts

Details Orbit design and perturbation analysis for Mars rover and sample return mission concepts Orbit design and perturbation analysis for Mars rover and sample return mission concepts

Jan 1989

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1989aiaa.meetu....k&link_type=abstract

AIAA, Aerospace Sciences Meeting, 27th, Reno, NV, Jan. 9-12, 1989. 13 p.

Physics

Mars Probes, Mars Sample Return Missions, Mars Surface Samples, Mission Planning, Orbit Calculation, Orbit Perturbation, Spacecraft Orbits, Interplanetary Flight, Radio Relay Systems, Roving Vehicles, Spacecraft Communication, Spacecraft Trajectories

Scientific paper

Mission options using out-of-orbit entry and Mars orbit rendezvous before earth return are discussed. The following major flight elements are required to conduct a Mars rover and sample return mission: the rover, the sample return orbiter, and the Mars ascent vehicle. The effects of perturbations on orbital motion are studied using Cowell's method and an averaging technique.

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