ハイブリッドラムジェットの理論性能検討
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概要
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Hybrid-ramjet is proposed in this paper. It is the combined engine of a liquid fuel ramjet and a ducted rocket. The high Isp performance and the wide fuel flow control range of a liquid fuel ramjet and the high combustion stability of a ducted rocket are expected. Theoretical calculations of the hybrid-ramjet which has same mass solid fuel and liquid fuel, were conducted. The results shows 50% higher Isp and twice fuel control range compared with a ducted rocket.
- 社団法人 日本航空宇宙学会の論文
- 2006-01-05