A feasibility study was performed that identified and characterized promising chemical propulsion system designs that utilize two or more of the propellant combinations: LOX/H2, LOX/CH4 and LOX/CO. The engine systems examined focused on the usage of common subsystem/component hardware where feasible. From the evaluation baseline employed, tripropellant MTV LOX cooled and bipropellant LEV and MEV engine systems are identified.
Engine system assessment study using Martian propellants
01.07.1992
Aufsatz (Konferenz)
Keine Angabe
Englisch
Engine System Assessment Study Using Martian Propellants
NTIS | 1992
|Engine system assessment study using Martian propellants
AIAA | 1992
|Engine system assessment study using Martian propellants
NTRS | 1992
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NTRS | 1989
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