Propellant requirements for military, commercial and research rocket; how to make usable propellants that do not meet freezing point requirements by use of additives such as ammonium thiocyanate added to hydrazine or water to hydrogen peroxide; nontoxic requirements; size of combustion chamber and injection arrangement; high thermal stability; approximate qualities of some of today's propellants.


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    Titel :

    Liquid propellants for manned rocket aircraft


    Weitere Titelangaben:

    Missiles Rockets


    Beteiligte:
    Mitchell, W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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