Abstract
1 Summerfield, M., A Theory of Unstable Combustion in Liquid Propellant Systems, ARS Journal, Vol. 21, No. 5, Sept. 1951, pp. 108-114. 2 Crocco, L., Aspects of Combustion Stability in Liquid Propellant Motors, Part 1, ARS Journal, Vol. 21, No. 6, Nov. 1951, pp. 163-178. 3 McKenna, K. J., Walker, J. H., and Winje, R. A., EngineAirframe Coupling in Liquid Systems, Journal of Spacecraft and Rockets, Vol. 2, No. 2, March-April 1965, pp. 254256. 4 Rubin, S., Longitudinal Instability of Liquid Rockets Due to Feedback (POGO). Journal of Spacecraft and Rockets, Vol. 3, No. 8, Aug. 1966, pp. 1188-1195. 5 Savant, C. J., Jr., Basic Feedback Control System Design McGraw-Hill, New York, 1958, pp. 124-168. 6 MacLean, D. I. and Wagner, H. Gg, Structure of the Reaction Zones of Ammonia-Oxygen and Hydrazine-Decomposition Flames, Eleventh Symposium (International) on Combustion, The Combustion Institute, 1967, p. 871. 7 Kestin, A. S., Turbulent Diffusion of Heat and Mass in Catalytic Reactors for Hydrazine Decomposition, Journal of Spacecraft and Rockets, Vol. 7, No. 1, Jan. 1970, pp. 31-36. 8 Dynamic Analyses of Thrust Chambers, Interim Rept. 4600-147-1, Sept. 1968, Walter Kidde & Co., Belleville, New Jersey. 9 Crocco, L., Grey, J., and Matthews, G. B., Measurements of the Combustion Time Lag in a Liquid Bipropellant Motor, Jet Propulsion, Vol. 26, No. 1, Jan. 1956, pp. 20-25. 10 Barrere, M., et al., Rocket Propulsion Van Nostrand, Princeton, 1960, pp. 630-632.
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