Stabilization of a bipropellant liquid rocket motor

Stabilization of a bipropellant liquid rocket motor

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The unstable burning of a bipropellant rocket combustion chamber is investigated and a study made of the requirements for an automatic closed loop control circuit to stabilize the motor. The bipropellant combustion chamber equations developed by Dr. L. Crocco(1) are utilised as the analytical descr...

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Bibliographic Details
Main Author: Cox, Dale W.
Format: Others
Published: 1952
Online Access:https://thesis.library.caltech.edu/1030/1/Cox_dw_1952.pdf
Cox, Dale W. (1952) Stabilization of a bipropellant liquid rocket motor. Engineer's thesis, California Institute of Technology. doi:10.7907/4SBW-M406. https://resolver.caltech.edu/CaltechETD:etd-03192009-154303 <https://resolver.caltech.edu/CaltechETD:etd-03192009-154303>

Internet

https://thesis.library.caltech.edu/1030/1/Cox_dw_1952.pdf
Cox, Dale W. (1952) Stabilization of a bipropellant liquid rocket motor. Engineer's thesis, California Institute of Technology. doi:10.7907/4SBW-M406. https://resolver.caltech.edu/CaltechETD:etd-03192009-154303 <https://resolver.caltech.edu/CaltechETD:etd-03192009-154303>

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