Mars Observer mission planning and systems design

Details Mars Observer mission planning and systems design Mars Observer mission planning and systems design

Jan 1989

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

AIAA, Aerospace Sciences Meeting, 27th, Reno, NV, Jan. 9-12, 1989. 14 p.

Computer Science

Mars Observer, Mission Planning, Spacecraft Control, Spacecraft Trajectories, Systems Engineering, Transfer Orbits, Data Acquisition, Spacecraft Launching, Upper Stage Rocket Engines

Scientific paper

The Mars Observer spacecraft, scheduled for launch in the Autumn of 1992, is a three-axis-stabilized platform carrying a payload for the investigation of the Martian surface, atmosphere, and gravitational and magnetic fields. Mission planning tasks encompass spacecraft trajectory design and both onboard and on-ground planning; five mission phases have been defined, namely launch, cruise, orbit-insertion, mapping, and quarantine. Scientific data-gathering functions will proceed autonomously throughout the two-year mapping mission.

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