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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    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    24 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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