Potential performance of a nuclear thermal rocket engine utilizing Martian CO2 as propellant
27th Joint Propulsion Conference ; 1991 ; Sacramento , CA , U.S.A.
1991-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Advanced Performance, Liquid Propellant, Rocket Engine
AIAA | 2005
|Engineering Index Backfile | 1961
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