Study on Combustion Dynamic Characteristics of Oxygen-Rich Preburners-Reference-Cited by-同舟云学术

Study on Combustion Dynamic Characteristics of Oxygen-Rich Preburners

Author:

Moon Il-Yoon¹,Kang Sang Hun²,Lee Soo-Yong³,Seo Seonghyeon⁴

Affiliation:

1. Rocket Engine Team, Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea

2. Department of Aerospace System Engineering, Sejong University, Seoul 143-747, Republic of Korea

3. Rocket Engine Development Division, Korea Aerospace Research Institute, Daejeon 305-333, Republic of Korea

4. Department of Mechanical Engineering, Hanbat National University, Daejeon 305-719, Republic of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

Reference26 articles.

1. HarrjeD. T.ReardonF. H. (eds.), “Liquid Propellant Rocket Combustion Instability,” NASA SP-194, 1972.

2. CroccoL.ChengS.I. “Theory of Combustion Instability in Liquid Propellant Rocket Motors,” AGARDograph 8, Butterworths Scientific, London, 1956.

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