A Mars orbiter mission design

Details A Mars orbiter mission design A Mars orbiter mission design

Aug 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992wadc.iafcu....c&link_type=abstract

IAF, International Astronautical Congress, 43rd, Washington, Aug. 28-Sept. 5, 1992. 6 p.

Mathematics

Dynamical Systems

Earth-Mars Trajectories, Manned Mars Missions, Swingby Technique, Circular Orbits, Computer Programs, Dynamical Systems, Space Missions

Scientific paper

A preliminary study of a new orbiter mission to Mars using an earth gravity assist is presented. The trajectory resulting from this study has been evaluated utilizing Everhart's (1985) integrator RADAU. The mission sequences are described and compared to other proposed mission designs and some mission opportunities for the years 1997 to 2014 are discussed.

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