References
- Bastress. E. K., 1961, 'Modification of the Burning Rates of Ammonium Perchlorate Solid Propellants by Particle Size Control,' Ph.D. Thesis, Princeton University, Princeton, New Jersey
- Beckstead, M.W., Derr, R.L., and Price, C. F. 1970, 'A Model of Composite Solid Propellant Combustion Based on Multiple Flames,' AIAA J. Vol. 8,2200
- Boyers, C., and Klayer, K., 1969, Propellant Manufacture, Hazards and Testings, American Chemical Society, Washington, D.C., Chap. 9
- Brewster, Q., and Son., S. F., 1995, 'Quasi-Steady Combustion Modelling of Homogeneous Solid Propellant,' Combustion and Flame Vol. 103, pp. 11-26 https://doi.org/10.1016/0010-2180(95)00075-H
- Cohen, N.S., Fleming, R.W., and Derr, R.L., 1974, 'Role of Binders in Solid Propellant Combustion,' AlAA J. 12, 212
- Crow, A.D., and Grimshaw, W. E., 1932, 'The combustion of colloidal propellant,' Trans., Kay. Soc. London, A230, 387 https://doi.org/10.1098/rsta.1932.0011
- Hightower, J.D., and Price, E.W., 1967, 'Combustion of Ammonium Perchlorate,' Xl Sysposium (International) on Combustion. Combustion Institute. Williams and Wilkens. Baltimore, Md., 463
- Hur, B.K., and Mok, Y.I., 1984, 'A New Approach to the Burning Rate Correlation of Solid Propellants,' HWAHAK KONGHAK Vol. 22, No. 1, pp. 51-58
- Kishore, K., Pai Verneker, V.R., and Nair, M. N. R, 1975, 'Condensed-phase reactions in solid propellants,' AlAA J. Vol. 13, 1240
- Kishore, K., 1979, 'Comprehensive View of the Combustion Models of Composite Solid Propellants,' AIAA J. Vol. 17, 1216
- Manelis, G.B., and Strunin, V.A., 1975, 'Mechanism and Elementary Theory of Burning of Composite Solid Propellants,' Proceedings of Inst-Symp. Space Technol. Sc., 97
- Morisaki, S., and Kornarniya, K., 1975, 'Differential Thermal Analysis and Thermogravimetry of Ammonium Perchlorate at Pressures up to 51 atm,' Thermochimica Acta Vol. 12,239 https://doi.org/10.1016/0040-6031(75)85037-4
- Nachbar, W., and Narks, T. M., 1957, 'A Sandwich Burner Model for the Composite Solid Propellants,' LMSO, 2191, AFOSR TN DD 132
- Rastogi, R.P., Singh, H.J., Deepak, D. and Strivastava., A.K., 1978, 'Pressure Dependence of Burning Rate of Composite Solid Propellants,' AIAA Vol. 16, No.5, pp. 534-536
- Rastogi, R.P., Kishore, K., and Singh, G., 1975, 'Solid Propellant Decomposition Studies by Differential Scanning Calorimetry,' Thermochimica Acta Vol. 12,89 https://doi.org/10.1016/0040-6031(75)85012-X
- Schultz, R.D., and Dekker, A.O., 1952, Aerojet General Corp., Rept. No. 576, Vol.1, Azusa, Calif. pp. 6-10
- Su, G.-J., 1946, Ind. Eng. Chem. Vol. 38, 803 https://doi.org/10.1021/ie50440a018
- Summerfield, M., Sutherland, G.S., Webb, M.J., Tabock, H.H., and Hall, K. P., 1960, 'The Burning Mechanism of Ammonium Perchlorate Propellants,' Solid Propellant Rocket Research Progress in Astronautics and Rocketry, New York, Vol. 1, pp. 141-182
- Sutherland, G.S., 1958, 'The Mechanism of Combustion of an Ammonium Perchlorate-Polyester Resin Composite Solid Propellant,' Ph. D. Thesis, Princeton University, Princeton, New Jersey
- Waesche, R.H. W., and Wenograd, J., 1967, 'The Effect of Pressure and Additives on the Kinetics of Decomposition of AP,' United Aircraft Research Lab., East Hartford, Conn., Rept. No. WSCI-67-8
- Waesche, R.H. W., and Wenograd, J., 1969, 'Calculation of Solid Propellant Burning Rate from Condensed-Phase Decomposition Kinetics,' AIAA Paper 69-145, New York, N. Y.
- Yoon, J.K., 1993, 'Prediction of Longitudinal Combustion Instability in a Solid-Propellant Rocket Motor,' KSME Journal, Vol. 8, No.2, pp, 206-213