The invention comprises a space ship, which commutes between earth orbit and lunar orbit, and is powered by a rocket engine, using superheated steam, or other non-cryogenic propellant, where the propellant is heated in a conventional uranium nuclear reactor.


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    Title :

    Thermal-nucleak powered rocket using non-cryogenic propellant


    Contributors:

    Publication date :

    2017-05-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke





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