Lifting entry and terminal phase system optimization for 1975 Mars Viking lander, considering graphical tradeoff approach including design parameter and atmosphere model variations
A technique for lifting entry and terminal phase system optimization for the 1975 Mars Viking lander
GUIDANCE, CONTROL AND FLIGHT MECHANICS CONFERENCE ; 1971 ; HEMPSTEAD, NY
01.08.1971
Aufsatz (Konferenz)
Keine Angabe
Englisch