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Performance Characteristics of GCH4-LOx Small Rocket Engine According to the Equivalence Ratio Variation at a Constant Pressure of Combustion Chamber

Journal of the Korean Society of Propulsion Engineers Pub Date : 2022-12-31 DOI:10.6108/kspe.2022.26.6.034
Y. Kang, H. Ahn, C. Bae, J. S. Kim
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GCH4-LOx小型火箭发动机在燃烧室恒压下等效比变化的性能特性
本文章由计算机程序翻译，如有差异，请以英文原文为准。
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Journal of the Korean Society of Propulsion Engineers
Journal of the Korean Society of Propulsion Engineers
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