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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    Titel :

    Pulse operated bipropellant reaction control valves


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Bailey, R.F. (Autor:in)

    Kongress:

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



    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Pulse Operated Bipropellant Reaction Control Valves

    Bailey, Roderick F. | SAE Technical Papers | 1965



    Internally vented bipropellant valves for divert and ACS missile control

    Cory, Jr., John / Farrell, Jr., William | AIAA | 1996


    Internally Vented Bipropellant Valves for Divert and ACS Missile Control

    Cory, J. M. / Farrell, W. F. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1996