Reasons for selection of molten lithium as fuel for investigation at General Motors Co and use of hydrogen peroxide as oxidizer; test facility consisted of enclosed, converted jet engine test cell; results of 36 bipropellant runs; it is found that rocket motor performance of lithium may be experimentally examined in simple all-liquid system; lithium-decomposed H2O2 reaction is shown to be hypergolic, stable, and controllable.


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    Titel :

    Research rocket testing of liquid lithium-hydrogen peroxide system


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Hardin, M.C. (Autor:in) / Masters, A.I. (Autor:in) / Toole, L.E. (Autor:in)

    Kongress:

    SAE Meeting ; 1961 Propellants



    Erscheinungsdatum :

    1961


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Research Rocket Testing of the Liquid Lithium-Hydrogen Peroxide System

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