Asteroid mission with maneuvers near Venus, earth, Mars, and Jupiter

Details Asteroid mission with maneuvers near Venus, earth, Mars, and Jupiter Asteroid mission with maneuvers near Venus, earth, Mars, and Jupiter

Jun 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993kosis..31...91l&link_type=abstract

Kosmicheskie Issledovaniya (ISSN 0023-4206), vol. 31, no. 3, p. 91-101.

Physics

Asteroid Missions, Circular Orbits, Earth (Planet), Jupiter (Planet), Mars (Planet), Venus (Planet), Asteroid Belts, Trojan Orbits

Scientific paper

Mission duration and energy requirements are estimated for expeditions to main-belt asteroids and Trojans with maneuvers near Venus, earth, Mars, and Jupiter. The most efficient mission routes are identified. Maximum energy requirements are estimated at 13.5 km/s for missions to main-belt asteroids and 15 km/s for missions to Trojans. The validity of the estimates of energy requirements is supported by calculations allowing for real orbit elements and planet and asteroid configurations for the period 1980-2020.

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