Affiliation:
1. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Reference8 articles.
1. Tôyama S. "High-Temperature Thermal Analysis on Nozzle of Thrust Chamber," AIAA paper 2002-2254,(2002)
2. Miyajima H. etal, "Performance of a Low-Thrust LO2/LH2 Engine with a 300:1 Area Ratio Nozzle," AIAApaper83-1313,(1983)
3. Sekita R. "The LE-5 Series Development, Approach to Higher Thrust, Higher Reliability, and GreaterFlexibility,"AIAApaper2000-3453,(2000)
4. Fujita M. etal, "Upper-Stage Propulsion System for H- ‡U A Launch Vehicle," AIAA paper 2002-4212,(2002)
5. Sutton G.P. and Biblarz, "Rocket propulsion Elements," Wiley International, pp.308pp.320, (2001)
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