Abstract

quencies, and Flame, Vol. 10, No. 4, Dec. 1966, pp. 367-380. 8 Oberg, C. O., Combustion Instability: Relationship Between and Nonacoustic Instability, AIAA Journal, Vol. 6, No. 2, Feb. 1968, pp. 265-271. 9 Culick, F. E. C., Some Non-Acoustic Instabilities in Rocket Chambers Are Acoustic, AIAA Journal, Vol. 6, No. 7, July 1968, pp. 1421-1423. 10 Culick, F. E. C., Acoustic Oscillations in Solid Propellant Rocket Chambers, Astronautica Ada, Vol. 12, No. 2, 1966, pp. 113-126. 11 T-Burner Manual, CPIA Publ. 191, Nov. 1969, Interagency Chemical Rocket Propulsion Group, Chemical Propulsion Information Agency, Silver Spring, Md. 12 Experimental Studies on the Oscillatory of Solid Propellants, NWC TP 4393, March 1969, Aerothermochemistry Division, Naval Weapons Center, China Lake, Calif. 13 Horton, M. D., Testing the Stability of Solid Propellants; Techniques and Data, ttOTS TP 3610, Aug. 1964, U. S. Naval Ordnance Test Station, China Lake, Calif; also Horton, M. D. and Price, E. W., Dynamic Characteristics of Solid Propellant Ninth Symposium (International) on Combustion, Academic Press, New York, 1963, pp. 303310. 14 Beckstead, M. W., Low Frequency Instability: A Comparison of Theory and Experiment, and Flame, Vol. 12, No. 1, Oct. 1968, pp. 417-426. 15 Fowling, J. and Smith, W. A. W., The Surface Temperatures of Ammonium Perchlorate Burning at Elevated Pressures, Tenth Symposium (International) on Combustion, Institute, Pittsburgh, Pa., 1965, pp. 1373-1380. 16 Culick, F. E. C., Calculation of the Admittance Function for a Burning Surface, Astronautica Ada, Vol. 13, No. 3, MayJune 1967, pp. 221-238. 17 Beckstead, M. W. and Boggs, T. L., The Effect of Oxidizer Particle Size on Nonacoustic Instability, 4th Conference, Interagency Chemical Rocket Propulsion Group, Chemical Propulsion Information Agency, CPIA Publ. No. 162, Vol. 1, Silver Spring, Md., Dec. 1967, pp. 337-346. 18 Culick, F. E. C., Some Problems in the Unsteady Burning of Solid Propellants, NWC TP 4668, Feb. 1969, Naval Weapons Center, China Lake, Calif.

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