Stability and Control of Liquid Propellant Rocket Systems
Author:
Affiliation:
1. Aerojet Engineering Corporation, Azusa, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.4544
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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