The take off orbit and its consequences on orbit mechanics and mission planning are examined. Based on an idealized preliminary investigation, orbit computation is realized and evaluated for Earth Mars orbits. The developed algorithm includes complex conical sections, impulse Hohmann transfer stations, Lambert problem and parameter optimization. Growth factors are to be included for the Space Station, in the next interplanetary missions.
Raumsimulation als Bahnhof fuer Interplanetare Missionen (Space Station as a Station for Interplanetary Missions)
1989
109 pages
Report
No indication
English
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