The launch window processor in the IGOS program, a sophisticated multipurpose space mission planning program, is presented. The specific problem of launch window analysis using the velocity matching model, that is for missions having fixed impulse upper stage motors with a target mission orbit plane, is discussed in some detail.
LAUNCH WINDOW ANALYSIS USING THE IGOS PROGRAM
Sae Technical Papers
SAE Aerospace Technology Conference and Exposition ; 1986
1986-10-01
Aufsatz (Konferenz)
Englisch
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