Stability and Control of Liquid Propellant Rocket Systems

Author:

LEE Y. C.1,GORE M. R.1,ROSS C. C.1

Affiliation:

1. Aerojet Engineering Corporation, Azusa, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Reference12 articles.

1. "A Theory of Unstable Combustion in Liquid Propellant Rocket Systems," by M . Summerfield,JOURNAL OF THE A M E R I - CAN R O C K E T SOCIETY, vol.21, September 1951, pp.108-114.

2. 'Aspects of Combustion in Liquid Propellant Rocket Motors, P a r t 1: Fundamentals. Low Frequency Instability With Monopropellants," by L. Crocco,JOURNAL OF THE A M E R I - CAN R O C K E T SOCIETY, vol.21, November 1951, pp.163-178.

3. "Servo-Stabilization of Low-Frequency Oscillations in a Liquid Bipropellant Rocket Motor," by Frank E . Marble and Dale W. Cox, Jr., Daniel and Florence Guggenheim J e t Propulsion Center,California Institute of Technology, Pasadena, Calif, (see pp.63-74in this issue of the JOURNAL).

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