Entry into orbit of planet may be assisted by entry into suitable satellite orbit around planet; circular satellite orbits for minimum energy are determined for planets of Solar System, assuming transfer along minimum energy semi-ellipse from Earth; effect is of practical interest for flights to Mercury and Mars.
Minimum energy entry into planetary satellite orbits
Brit Interplanetary Soc -- J
British Interplanetary Society -- Journal ; 18 , n 2
1961
3 pages
Aufsatz (Zeitschrift)
Englisch
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Entry into circular planetary satellite orbits
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