The patent application describes an igniter for use in a rocket having a predetermined spin rate during flight. The rocket includes a plurality of motors facing out from the body of the rocket and each motor is fired in a predetermined sequence. The igniter includes a squib for igniting fine black powder in the cavity of the igniter. The powder is packed in the cavity of the igniter with the density substantially like a cake. A cover member retains the powder in the cavity for a sufficient time to achieve fast ignition. (Author)


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    Titel :

    Rocket Motor Igniter for Precision Centroid of Thrust


    Beteiligte:
    R. E. Betts (Autor:in) / N. P. Williams (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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