A review is given of the performance of 98 percent H2O2 in bipropellant systems, in hybrid rockets, as a monopropellant, and as a secondary injection fluid. In addition, extensive data are given on the propellant's heat transfer characteristics, storability, radiation resistance, and materials compatibility. (Author)


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    Title :

    The 98% H2O2 Monomethyl Hydrazine Propeliant Combination and Its Suitability for the Gemini Spacecraft Attitude Control System


    Contributors:

    Publication date :

    1963


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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