RESEARCH PAPERS
Miller, W. H., Burkes, W. M., and McClendon, S. E., “Design approach for variable flow ducted rockets,” AIAA/SAE/ASME 17th Joint Propulsion Conference, Colorado, USA, Jul 1981.
10.2514/6.1981-1489Fry, R. S., “A Century of Ramjet Technology Propulsion Evolution,” Journal of Propulsion and Power, Vol. 20, No. 1, 2004, pp. 27-58.
10.2514/1.9178Sung, H. G., and Yoon, H. G., “Technical Review and Analysis of Ramjet/Scramjet Technology : Ⅰ. Ramjet Engine(Liquid Ramjet, Ducted Rocket),” Journal of the Korean Society of Propulsion Engineers, Vol. 10, No. 1, 2006, pp. 72-86.
Komornik, D., and Gany, A., “Study of a Hybrid Gas Generator for a Ducted Rocket,” Combustion, Explosion, and Shock Waves, Vol. 53, No. 3, 2017, pp. 293-297.
10.1134/S0010508217030066Komornik, D., and Gany, A., “Investigation of a Ducted Rocket with a Paraffin/Oxygen Hybrid Gas Generator,” Journal of Propulsion and Power, Vol. 35, No. 6, 2019, pp. 1108-1115.
10.2514/1.B37448Ryu, S. H., Han, S. J., Kim, K. H., Kim, J. K., and Moon, H. J., “Experimental Investigation of Gas Nitrous Oxide / Paraffin Hybrid Gas Generator for Ducted Rocket,” Asian Joint Conference on Propulsion and Power, Kagawa, Japan, Mar 2016.
Han, S. J., Ryu, S. H., Kim, J. K., Kang, T. G., Moon, H. J., Kim, J. H., and Ko, S. W., “Fuel Rich Gas O/F Ratio Characteristics of HDPE and Paraffin Fuel in Low Range of the Oxidizer Mass Flux,” Journal of the Korean Society of Propulsion Engineers, Vol. 20, No. 6, 2016, pp. 54-60.
10.6108/KSPE.2016.20.6.054Whitmore, S. A., Walker, S. D., Merkley, D. P., and Sobbi, M., “High Regression Rate Hybrid Rocket Fuel Grains with Helical Port Structures,” Journal of Propulsion and Power, Vol. 31, No. 6, 2015, pp. 1727-1738.
10.2514/1.B35615Walker, S. D., “High Regression Rate Hybrid Rocket Fuel Grains with Helical Port Structures,” Master Thesis, Aerospace Engineering, Utah State University, Logan, Utah, USA, 2015.
Sigalotti, L. D. G., Alvarado-Rodríguez, C. E., and Rendón, O., “Fluid Flow in Helically Coiled Pipes,” Fluids, Vol. 8, No. 12, 2023.
10.3390/fluids8120308Marxman, G., and Gilbert, M., “Turbulent Boundary Layer Combustion in The Hybrid Rocket,” Symposium (International) on Combustion, Vol. 9, No. 1, 1963.
10.1016/S0082-0784(63)80046-6Humble, R. W., Henry, G. N., and Larson, W. J., Space Propulsion Analysis and Design, McGraw-Hill Inc., New York, NY, USA, Ch. 7, 1995.
- Publisher :The Korean Society of Propulsion Engineers
- Publisher(Ko) :한국추진공학회
- Journal Title :Journal of the Korean Society of Propulsion Engineers
- Journal Title(Ko) :한국추진공학회지
- Volume : 30
- No :4
- Pages :73-81
- Received Date : 2026-05-05
- Revised Date : 2026-07-10
- Accepted Date : 2026-07-15
- DOI :https://doi.org/10.6108/KSPE.2026.30.4.073


Journal of the Korean Society of Propulsion Engineers








