Use of a sampling feedback system for stabilization of low frequency oscillations in liquid monopropellant rocket motors
Instability in liquid monopropellant rocket motors may be corrected by the use of a feedback servomechanism. This mechanism consists essentially of a pressure pickup which senses pressure oscillations in the combustion chamber, an amplifier and a variable capacitance in the feed line. It is shown th...
Internet
https://thesis.library.caltech.edu/1462/1/Fernandez%2CC_1953.pdfFernandez, Raymond Caesar (1953) Use of a sampling feedback system for stabilization of low frequency oscillations in liquid monopropellant rocket motors. Engineer's thesis, California Institute of Technology. doi:10.7907/PZEC-N445. https://resolver.caltech.edu/CaltechETD:etd-04232003-090202 <https://resolver.caltech.edu/CaltechETD:etd-04232003-090202>