Funder
National Research Foundation of Korea
Reference22 articles.
1. E. Betts, R. Frederick, A historical systems study of liquid rocket engine throttling capabilities, in: 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2010, p. 6541.
2. R. Gilroy, R. Sackheim, The lunar module descent engine-A historical summary, in: 25th Joint Propulsion Conference, 1989, p. 2385.
3. G. Dressler, J. Bauer, TRW pintle engine heritage and performance characteristics, in: 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2000, p. 3871.
4. Liquid-propellant rocket engine throttling: a comprehensive review;Casiano;J. Propul. Power,2010
5. Effects of momentum ratio and weber number on spray half angles of liquid controlled pintle injector;Son;J. Therm. Stresses,2015
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