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.
Servo-stabilization of low-frequency oscillations in liquid bipropellant rocket motor
Am Rocket Soc -- J
American Rocket Society -- Journal ; 23 , n 2
1953
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Article (Journal)
English
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