Flight trajectory to Jupiter using the gravitational field of Mars

Details Flight trajectory to Jupiter using the gravitational field of Mars Flight trajectory to Jupiter using the gravitational field of Mars

Jan 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978kosis..16...38g&link_type=abstract

Kosmicheskie Issledovaniia, vol. 16, Jan.-Feb. 1978, p. 38-43. In Russian.

Physics

Earth-Mars Trajectories, Interplanetary Trajectories, Jupiter (Planet), Swingby Technique, Trajectory Optimization, Energy Consumption, Launch Windows, Time Dependence

Scientific paper

A method of calculating minimum power-consumption for earth-Mars-Jupiter trajectories is proposed for the period extending from 1979 to 1990. The influence of the swingby conditions and of the year in which the spacecraft is launched on the trajectory parameters and the effectiveness of correction maneuvers at various flight stages is analyzed. The savings in power consumption provided by the swingby maneuver are shown to depend strongly on the year in which the launch occurs.

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