Maximum payload is required for given vehicle; in variation problem, equations of movement of space vehicles occur as secondary condition; further conditions enter problem by technical limitations of propulsion; limiting cases of unbounded and constant thrust are considered; in both cases distinction must be made between flights with given time of takeoff in synodic year and those with open time of takeoff; time will be chosen so that payload becomes maximum.
Optimization of interplanetary flights with vehicles of low thrust acceleration
Zur Optimalisierung interplanetarer Uebergangsbahnen mit kleiner Schubbeschleunigung
Raketentechnik u Raumfahrtforschung ; 7 , n 4
1963
5 pages
Aufsatz (Zeitschrift)
Deutsch
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Optimization of interplanetary flights with vehicles of low thrust acceleration
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