The rocket motor has a plurality of jets spaced around the rocket chamber for providing a reverse thrust. The rocket motor has an axial nozzle. Air pressure entering the nose of the rocket is used to activate an electric circuit to open the thrust reversal nozzles. The operation of the reversal nozzles aids in separating the rocket motor from the forward missile portion.


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    Titel :

    Thrust Reversal Unit for Rocket Motor


    Beteiligte:
    R. G. Daudelin (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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