A comparative analysis of three-impulse trajectories that are optimum for limitations on time of transfer and on the maximum distance from the planet

Details A comparative analysis of three-impulse trajectories that are optimum for limitations on time of transfer and on the maximum distance from the planet A comparative analysis of three-impulse trajectories that are optimum for limitations on time of transfer and on the maximum distance from the planet

Jul 1980

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980cosre..18....7i&link_type=associated

(Kosmicheskie Issledovaniia, vol. 18, Jan.-Feb. 1980, p. 11-21.) Cosmic Research, vol. 18, no. 1, July 1980, p. 7-16. Translati

Physics

Interplanetary Spacecraft, Planetary Orbits, Spacecraft Trajectories, Trajectory Optimization, Transfer Orbits, Distance, Elliptical Orbits, Radial Velocity, Transit Time

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