Mission and Vehicle Sizing Sensitivities
Mission and Vehicle Sizing Sensitivities
- New search for: A. C. Young
- New search for: A. C. Young
Representative interplanetary space vehicle systems are sized to compare and show sensitivity of the initial mass required in low Earth orbit to one mission mode and mission opportunity. Data are presented to show the requirements for Earth-Mars opposition and conjunction class roundtrip flyby and stopover mission opportunities available during the time period from year 1997 to year 2045. The interplanetary space vehicle consists of a spacecraft and a space vehicle acceleration system. Propellant boil-off for the various mission phases is given for the Lox/LH (Liquid Oxygen/Liquid Hydrogen) propulsion systems. Mission abort information is presented for the 1999 Venus outbound swingby trajectory, transfer profile.
Document information
Mission and Vehicle Sizing Sensitivities
1986
16 pages
Report
No indication
English
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