System, developed to provide control at high altitudes in regions of low dynamic pressure and to operate at zero normal acceleration and in extremely low-temperature environment, consists of storage vessel, pressurization system, flow control system, and rocket units; on-off control is used with which rockets are operated at fixed thrust levels of from 20 to 40 lb; problems encountered, fabrication of system, and data pertinent to performance characteristics.


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    Titel :

    Hydrogen-peroxide rocket reaction-control system for X-1b research airplane


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Love, J.E. (Autor:in) / Stillwell, W.H. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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    Research Rocket Testing of the Liquid Lithium-Hydrogen Peroxide System

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