Millions of lbs of thrust required to launch large space vehicles can be obtained by using large solid-propellant rocket motors; method presented for loading castable solid propellants into large launching units in position at launching sites; include potential site location, motor shell erection, etc.


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    Title :

    On-site loading of solid propellants for large missile and satellite launching units


    Additional title:

    ASME -- Paper


    Contributors:
    Haite, W.F. (author)

    Conference:

    ASME Meeting ; 1959 Launching



    Publication date :

    1959


    Size :

    4 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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