Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Reference7 articles.
1. 1) Huzel, D. K. and Huang, D. H.: Modern Engineering for Design of Liquid Propellant Rocket Engines, AIAA Publication, Washington DC, 1992.
2. 2) Yatsuyanagi, N., Gomi, H. and Sakamoto, H.: An Empirical Expression of the C* Efficiency of LOX/Hydrogen Rocket with Coaxial Injector, AIAA Paper 85-1387, 1985.
3. Study on Breakup Length of Liquid Jet by Liquid-Gas Coaxial Injector —Evaluation of Atomization Characteristics of Rocket Engine Injectors—
4. Study on the Design Criteria of the Coaxial Injector for a LOX/Hydrogen Rocket Engine —Evaluation of Design for Injectors of the LE-5 Engine and Its Derivatives—
5. 5) Design Report for RL 10A-3-3 Rocket Engine, Contact No. NAS8-15494, Pratt & Whitney Aircraft, 1966.
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