Interplanetary round-trip trajectory optimization - Round-Trip Delta-V (RTDV) plots

Details Interplanetary round-trip trajectory optimization - Round-Trip Delta-V (RTDV) plots Interplanetary round-trip trajectory optimization - Round-Trip Delta-V (RTDV) plots

Aug 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991ads..confr....h&link_type=abstract

AAS and AIAA, Astrodynamics Specialist Conference, Durango, CO, Aug. 19-22, 1991. 21 p.

Astronomy and Astrophysics

Astronomy

Flight Time, Interplanetary Trajectories, Parking Orbits, Round Trip Trajectories, Trajectory Optimization, Interplanetary Flight, Launch Windows, Manned Mars Missions, Transfer Orbits

Scientific paper

The Round-Trip Delta-V (RTDV) plot technique provides a quick and systematic method for initiating trajectory design for interplanetary round-trip missions. Features in typical RTDV plots are discussed for earth-Mars-earth missions, and sensitivities of such missions to launch date, stay time, and parking orbit characteristics are demonstrated. Midcourse maneuvers and free return constraint are included. Examples are also given for earth-Venus-earth and earth-Jupiter-earth missions.

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