Ephemeridal parameter optimization for minimum propellant requirements for round trip swingby- stopover multiplanet mission
Optimization of ''ephemeridal'' parameters for minimum propellant requirements on multiplanet roundtrip swingby-stopover missions.
ASTRODYNAMICS SPECIALIST CONFERENCE ; 1968 ; JACKSON, WY, US
01.09.1968
Aufsatz (Konferenz)
Keine Angabe
Englisch
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