The patent relates to an igniter mechanism for a rocket motor used for towing a load or extracting an air crew member from a disabled aircraft. The mechanism operates whenever a sufficient force is exerted on the tow line to shear a pin allowing closure of the switch. Electrical energy coupled to the switch is conducted to a squib which ignites a charge to cause ignition of the rocket motor propellant. The electrical switch mechanism can only be actuated by a predetermined pulling force on the tow line thereby causing the electrical contacts to be brought positively together.


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    Titel :

    Load Actuated Electro-Ignition Circuit Switch


    Beteiligte:
    J. A. Schmidt (Autor:in) / W. J. Stone (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Load Actuated Electro-Ignition Switch

    W. J. Stone | NTIS | 1974


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