Safety philosophies and techniques developed by NASA Wallops Station, Va, for storage, handling, assembly, and flight of rockets; emphasis is on most likely modes of motor ignition or detonation and those energy sources available to produce initiation; sounding-rocket flight safety is related to vehicle reliability, dispersion and wind sensitivity, as well as to mission objectives; method developed for qualifying vehicles for flight without flight termination system is described, along with functions provided to safety personnel by vehicle design review; methods for determining that probability of hitting land, ship, or aircraft will be less than 1×10-5, are presented.


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    Titel :

    Operational range safety for solid-propellant sounding rockets


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Parker, L.C. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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    BUSSE, J. / KREUZER, J. | AIAA | 1967


    Liquid propellant utilization for sounding rockets.

    Busse, J. R. / Kreuzer, J. A. | NTRS | 1967


    A FIRST STAGE SOLID PROPELLANT ROCKET MOTOR FOR SOUNDING ROCKETS

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