Response time of attitude control rockets for space vehicles is function of valve response; minimum obtainable impulse bit is influenced by propellant valve characteristics; design parameters to consider for valves include reliability, performance, material compatibility, and weight; reliability is obtained by simplicity of design; performance requirements are fast response, zero propellant leakage, simultaneous operation of fuel and oxidizer metering, and contamination tolerance; valve weight is minimized through use of torque motor; suitable materials are evaluated for compatibility with propellants.


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    Title :

    Pulse operated bipropellant reaction control valves


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    Proceedings of the SAE-NASA -- Aerospace Vehicle Flight Control Conference ; 1965 Control



    Publication date :

    1965


    Size :

    6 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Pulse Operated Bipropellant Reaction Control Valves

    Bailey, Roderick F. | SAE Technical Papers | 1965



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