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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    Title :

    Engine system assessment study using Martian propellants


    Contributors:
    Pelaccio, D. (author) / Jacobs, M. (author) / Collins, J. (author) / Scheil, C. (author) / Meyer, M. (author)

    Publication date :

    1992-07-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Engine system assessment study using Martian propellants

    Pelaccio, Dennis / Jacobs, Mark / Scheil, Christine et al. | NTRS | 1992


    Engine System Assessment Study Using Martian Propellants

    D. Pelaccio / M. Jacobs / C. Scheil et al. | NTIS | 1992


    Engine system assessment study using Martian propellants

    PELACCIO, D. / JACOBS, M. / COLLINS, J. et al. | AIAA | 1992