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.
Servo-stabilization of combustion in rocket motors
Am Rocket Soc -- J
American Rocket Society -- Journal ; 22 , n 5
1952
Article (Journal)
English
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