Research Article
Unmack, K. E., “Wide range thrust throttling of a solid rocket motor,” AIAA/SAE/ASME/ASEE Joint Propulsion Conference, Cincinnati, OH, USA, AIAA-87-2085, 1987.
Humble, R. W., Henry, G. N., and Larson, W. J., Space Propulsion Analysis and Design, McGraw-Hill, New York, NY, 1995.
Chiaverini, M. J., and Kuo, K. K., Fundamentals of Hybrid Rocket Combustion and Propulsion, AIAA, Reston, VA, pp. 4-7, 2007.
DeLuca, L. T., Shimada, T., and Sinditskii, V. P., Chemical Rocket Propulsion: A Comprehensive Survey of Energetic Materials, Springer, Cham, Switzerland, pp. 501-503, 2017.
10.1007/978-3-319-27748-6Heister, S. D., and Anderson, W. E., “Thrust modulation in solid rocket motors,” Journal of Propulsion and Power, Vol. 16, No. 2, 2000, pp. 172-180.
Lee, J., Shin, S., Han, J., Kim. S,, and Choi, H., “Pintle nozzle flow characteristics for variable thrust rocket motors,” Aerospace Science and Technology, Vol. 45, 2015, pp. 27-34.
Lengelle, G., “Solid propellant combustion,” Combustion Science and Technology, Vol. 96, Nos. 1-3, 1994, pp. 131-164.
Burroughs, S., “Status of army pintle technology for controllable thrust propulsion,” AIAA Joint Propulsion Conference, Salt Lake, UT, AIAA 2001-3598, 2001.
10.2514/6.2001-3598Summerfield, M., Sutherland, G. S., Webb, M. J., Taback, H. J., and Hall, K. P. “Burning mechanism of composite propellants,” in Solid Propellant Rocket Research, edited by M. Summerfield, Academic Press, New York, NY, pp. 141-182, 1960.
10.2514/5.9781600864766.0141.0182Price, E. W., Sigman, R. K., and Boggs, T. L., “Combustion of composite solid propellants,” Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, edited by V. Yang, T. B. Brill, and W. Z. Ren, AIAA, Reston, VA, pp. 112-115, 2000.
Culick, F. E. C., “Unsteady motions in combustion chambers for propellant rocket motors,” AGARD-AG-261, 1981.
Turns, S. R., An Introduction to Combustion: Concepts and Applications, 3rd ed., McGraw-Hill, New York, NY, 2012.
DeLuca, L. T., Galfetti, L., Maggi, F., Colombo, G., Reina, A., Tadini, P., and Bandera, A., “Energetic binders and plasticizers,” Propellants, Explosives, Pyrotechnics, Vol. 35, No. 5, 2010, pp. 387-397.
Gordon, S., and McBride, B. J., “Computer program for calculation of complex chemical equilibrium compositions and applications,” NASA RP-1311, 1994.
Kohga, M., Hagihara, Y., Hori, K., and Iwahashi, N., “Thermochemical analysis of NEPE propellants,” Propellants, Explosives, Pyrotechnics, Vol. 35, No. 6, 2010, pp. 493-501.
Meyer, R., Köhler, J., and Homburg, A., Explosives, 6th ed., Wiley-VCH, Weinheim, 2007.
10.1002/9783527617043Sellas, J. T., “A review of the parameters affecting the pressure exponent in composite solid propellants,” 17th International Annual Conference of ICT, 1986, pp. 14.1-14.15.
Han, S., Min, B. s., Yoon, J., Heo, J., and Ha, D., “Ground firing tests of standard motor and system sizing for long duration divert and attitude control system,” Journal of the Korean Society of Propulsion Engineers, in press.
Beckstead, M. W., “Overview of combustion mechanisms and flame structures for advanced solid propellants,” Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, edited by V. Yang, T. B. Brill, and W. Z. Ren, Vol. 185, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, pp. 3-35, 2000.
- Publisher :The Korean Society of Propulsion Engineers
- Publisher(Ko) :한국추진공학회
- Journal Title :Journal of Propulsion and Energy
- Journal Title(Ko) :Free Open Access International Journal on Propulsion and Energy Science and Technology
- Volume : 6
- No :1
- Pages :23-35
- Received Date : 2026-02-24
- Revised Date : 2026-04-01
- Accepted Date : 2026-04-05
- DOI :https://doi.org/10.6108/JPNE.2026.6.1.023
Journal of Propulsion and Energy
