Jupiter orbiter spacecraft propulsion system design, noting advantages of fluorine/hydrazine propellant combination
Propulsion subsystem design for Jupiter orbiter missions
ANNUAL MEETING ON JUPITER ORBITERS AND PROBES - A PRELIMINARY ASSESSMENT OF REQUIREMENTS ; 1971 ; SEATTLE, WA
1971-06-01
Conference paper
No indication
English
Orbit Design Concepts for Jupiter Orbiter Missions
AIAA | 1976
|Orbit design concepts for Jupiter orbiter missions
NTRS | 1974
|Orbit design concepts for Jupiter orbiter missions
AIAA | 1974
|