It is shown that combustion in rocket motor can be stabilized against any value of time lag in combustion by feedback servo link from chamber pressure pickup, through appropriately designed amplifier, to control capacitance on propellant feed line; technique of stability analysis is based upon combination of Satche diagram and Nyquist diagram.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Servo-stabilization of combustion in rocket motors


    Additional title:

    Am Rocket Soc -- J


    Contributors:
    Tsien, H.S. (author)

    Published in:

    Publication date :

    1952


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Combustion Instability in Solid Rocket Motors

    E. W. Price / G. A. Flandro | NTIS | 1989



    Combustion termination of solid rocket motors

    BROWNE, T. P. / DAY, E. E. / TABACK, H. J. | AIAA | 1965


    Model of Hybrid Rocket Combustion in Classical Hybrid Rocket Motors

    Morita, Takakazu / Yuasa, Saburo / Shimada, Toru et al. | AIAA | 2013