Recent work of H.S.TSIEN is extended to liquid bipropellant motor; by use of feedback system containing device to sense combustion chamber pressure, suitably designed amplifier, and servomechanism which governs propellant flow, low frequency oscillations which occur in rocket configuration may be stabilized for any value of combustion time lag.


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    Title :

    Servo-stabilization of low-frequency oscillations in liquid bipropellant rocket motor


    Additional title:

    Am Rocket Soc -- J


    Contributors:

    Published in:

    Publication date :

    1953


    Remarks:

    Diagrams


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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