Journal of the Korean Society of Propulsion Engineers ISSN:1226-6027(Print) 2288-4548(Online) 한국추진공학회지

Dressler, G.A., “Summary of Deep Throttling Rocket Engines with Emphasis on Apollo LMDE,“ 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, C.A., U.S.A., AIAA 2006-5220, Jul. 2006.

Gromski, J.M., Majamaki, A.N., Chianese, S.G., Weinstock, V.D. and Kim, T.S., “Northrop Grumman TR202 LOX/LH2 Deep Throttling Engine Technology Project Status,“ 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Nashville, T.N., U.S.A., M10-0843, Jul. 2010

Gerard W. Elverum, Jr. and Peter Staudhammer, “The Effect of Rapid Liquid-Phase Reactions on Injector Design and Combustion in Rocket Motors,” JPL, Progress Report No. 30-4, 25 August 1959.

Gordon, A., Dressler, J. and Bauer, M., “TRW Pintle Engine Heritage and Performance Characteristics,“ 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2000.

Casiano, M.J., Hulka, J.R. and Yang, V., “Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review,“ Journal of Propulsion and Power, Vol. 26, No. 5, pp. 897-923, 2010.

Kwak, H.D., Kwon, S.J. and Choi, C.H., “Performance Assessment of Electrically Driven Pump-fed LOX-kerosene Cycle Rocket Engine: Comparison with Gas Generator Cycle,“ Aerospace Science and Technology, Vol. 77, pp. 67-82, 2018.

Hwang, D.K., Kim, J.G., Kwon, S.J. and Choi, C.H., “Geometric Effects of Liquid Rocket Engine Pintle Injectors in Supercritical Condition,“ International Journal of Advanced Science and Technology, Vol. 23 pp. 941-952, 2022.

Kang, D.H., Hwang, D.H., Ryu, C.S., and Ko, Y.S., “Analysis of Pintle Tip Thermal Damage in the Combustion Hot Firing Test with a 1.5-tonf Class Liquid-Liquid Pintle Injector,” Journal of the Korean Society of Propulsion Engineers, Vol. 24, No. 6, pp.1-9, 2020.

Kang, D.H., Han, S.H., Ryu, C.S., and Ko, Y.S., “Design of pintle injector using Kerosene-LOx as propellant and solving the problem of pintle tip thermal damage in hot firing test,” Acta Astronautica, Vol. 201, pp. 48-58, 2022.

Kang, D.H., Kim, J.G., , Ryu, C.S., and Ko, Y.S., “Study on the High Pressure Combustion Performance Characteristics of the 1st Row Pintle Injector using LOx-Kerosene as Propellant” Journal of Aerospace System Engineering, Vol. 16, No. 5, pp.17-25, 2022.

Lei, J., Lan, X., Zhang, R. and Chen, Y., “The development of 7500N variable thrust engine for Chang’E-3,” Chinese Science, Vol 44, pp. 569-575, 2014.