Three dimensional orbit is worked out, in which vehicle approaches moon to within 11,000 km arriving at position from which hidden lunar hemisphere can be observed; in subsequent study launching site is chosen along Northern latitude; effects of application of retro-rocket in vicinity of moon; orbits planned to hit moon, circumnavigate moon and return to earth; possibility of launching moon satellite is examined. (In English; German and French abstracts).
On numerical computation of free trajectories of lunar space vehicle
Astronautica Acta
Astronautica Acta ; 6 , n 2-3
1960
29 pages
Aufsatz (Zeitschrift)
Englisch
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