Mars exploration mission

Details Mars exploration mission Mars exploration mission

Jul 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991fsa..workq....m&link_type=abstract

In NASDA, Future Space Activities Workshop: Lunar Base Workshop 1991 22 p (SEE N92-33753 24-91)

Physics

Interplanetary Transfer Orbits, Japanese Spacecraft, Mars (Planet), Mars Probes, Mission Planning, Orbital Mechanics, Space Exploration, Mars Excursion Module, Mars Landing, Mars Sample Return Missions, Spacecraft Design, Spacecraft Reentry

Scientific paper

Mars exploration scenarios are reviewed. An emphasis is placed on scientific exploration. The review and evaluation results are reported for the following items: (1) orbit plans for Mars surface exploration missions that begin in Low Earth Orbit (LEO); (2) powered and aerodynamic capturing payloads from the transfer orbit to a Mars revolving orbit; and (3) a penetrator system as a Mars landing vehicle. Proposed Mars transfer orbits have the following advantages over Hohmann orbits: (1) transfer time and angle are less; (2) the inclination between the orbital planes of Earth and Mars is considered; and (3) velocity variations are not required to change orbit plane.

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