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.
Pulse operated bipropellant reaction control valves
SAE -- Paper
Proceedings of the SAE-NASA -- Aerospace Vehicle Flight Control Conference ; 1965 Control
1965
6 pages
Conference paper
English
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Pulse Operated Bipropellant Reaction Control Valves
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