A Study on the Recess Optimization of LOx/CH4 Bi-swirl Injector through the Comparison of Spray and Combustion Performance

Author:

Kang Yun Hyeong,Bae Chang Han,Park Hong Yeong,Kim Jeong Soo

Funder

Ministry of Science and ICT, South Korea

National Research Foundation of Korea

Ministry of Trade, Industry and Energy

Korea Evaluation Institute of Industrial Technology

Publisher

The Korean Society of Propulsion Engineers

Reference17 articles.

1. Bicentrifugal Swirl Injector Development for Hydrogen Peroxide and Non-Toxic Hypergolic Miscible Fuels

2. Combustion Stability Characteristics of Coax-Swirl-Injectors for Oxygen/Kerosene

3. Dynamic Characterization of Double Swirl Injectors for GOX/Kerosene

4. Rubinsky, V. R., “Combustion Instability in the RD-0110 Engine,” Liquid Rocket Engine Combustion Instability, edited by W. E. Anderson and V. Yang, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, pp. 89-112, 1995.

5. Injector Head for RD-170 Engine Combustion Chamber

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