One Thiokol Chemical Corporation TE-M-364-19 solid-propellant rocket motor was fired while spinning at 60 rpm about its axial centerline. The motor was ignited at a simulated altitude of 122,000 ft, following temperature conditioning at 15 + or - 5 F for a minimum of 44 hr. The program objectives of determining vacuum ballistic performance, altitude ignition characteristics, motor temperature-time history, the lateral (nonaxial) thrust vector, and structural integrity of the motor components are presented and discussed. (Author)


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    Titel :

    Qualification Test of the Thiokol TE-M-364-19 Solid-Propellant Rocket Motor (S/N 19006)


    Beteiligte:
    H. L. Merryman (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    62 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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