Engine system assessment study using Martian propellants

Details Engine system assessment study using Martian propellants Engine system assessment study using Martian propellants

Jul 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992jpnt.confqt...p&link_type=abstract

AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit, 28th, Nashville, TN, July 6-8, 1992. 34 p.

Computer Science

Chemical Propulsion, Extraterrestrial Resources, Mars (Planet), Spacecraft Propulsion, Carbon Monoxide, Hydrogen, Liquid Oxygen, Methane

Scientific paper

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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