Possibilities for thermonuclear reactions to be used as energy source for propulsion of atomic rockets, photon rockets, turbojets, and ram jets; results indicate maximum heat production at 108 K for hydrogen isotopes. English translation from Astronautica Acta pt 2 1955.


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    Title :

    Steady nuclear combustion in rockets


    Additional title:

    NACA -- Tech Memo


    Contributors:
    Saenger, E. (author)


    Publication date :

    1957


    Size :

    39 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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