NASA NTRS · 19920071406
Engine system assessment study using Martian propellants
Abstract
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.
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Pelaccio, D., Jacobs, M., Collins, J., Scheil, C., Meyer, M.. 1992-07-01. Engine system assessment study using Martian propellants. https://ntrs.nasa.gov/citations/19920071406
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