The thruster is utilized in emergency aircraft escape systems. The gas from a propellant charge is used to effect the power stroke of the thruster and to provide the integral damping action. This involves the use of a combined high-low principle with dual driving faces and a single buffer face.


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    Titel :

    Damped Thrust


    Beteiligte:
    C. S. Sterrett (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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