Mars trajectory options for the Space Exploration Initiative

Details Mars trajectory options for the Space Exploration Initiative Mars trajectory options for the Space Exploration Initiative

Aug 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992asdy.conf.1935s&link_type=abstract

IN: Astrodynamics 1991; Proceedings of the AAS/AIAA Astrodynamics Conference, Durango, CO, Aug. 19-22, 1991. Pt. 3 (A92-43251 18

Astronomy and Astrophysics

Astronomy

Abort Trajectories, Earth-Mars Trajectories, Flyby Missions, Mission Planning, Round Trip Trajectories, Nuclear Propulsion, Space Exploration, Trajectory Planning

Scientific paper

The Mission Definition Office within the Lunar and Mars Exploration Program Office at the NASA/Johnson Space Center has the responsibility for leading the Space Exploration Initiative mission design activities across the Agency. In support of the Synthesis Group architecture analyses, a mission concept that includes fast one-way transits to and from Mars, a powered flyby abort, and an early return option has been developed. This paper will describe this integrated approach to Mars mission planning.

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