Some cases of interplanetary transfer, using a perturbation maneuver

Details Some cases of interplanetary transfer, using a perturbation maneuver Some cases of interplanetary transfer, using a perturbation maneuver

Sep 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974kosis..12..675i&link_type=abstract

Kosmicheskie Issledovaniia, vol. 12, Sept.-Oct. 1974, p. 675-681. In Russian.

Computer Science

Grand Tours, Interplanetary Transfer Orbits, Spacecraft Maneuvers, Swingby Technique, Trajectory Optimization, Earth-Mars Trajectories, Fuel Consumption, Gravitational Effects, Jupiter Project, Orbit Perturbation

Scientific paper

The analytical determination of power-optimal swing-by trajectories is studied, using some simplifying assumptions. An analytical solution obtained for an Earth-Jupiter trajectory involving a swing-by maneuver at the planet Mars is compared with a numerical solution, showing that the analytical results provide savings on the order of 1 km/sec in the characteristic velocity of the maneuver. The method proposed is readily adaptable to flights from large to small planets.

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