The First Russian LOX-LH2 Expander Cycle LRE: RD0146
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American Institute of Aeronautics and Astronautics
Cited by 13 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Comparative Analysis of Heat Flux Variation in LOx/GCH4 Ribbed Combustor with Different Rib Types;AIAA SCITECH 2024 Forum;2024-01-04
2. Flame dynamics of an injection element operated with LOX/H2, LOX/CNG and LOX/LNG in a sub- and supercritical rocket combustor with large optical access;International Journal of Spray and Combustion Dynamics;2023-05-19
3. Review and Development Trends for Expander Cycle Engine;Journal of the Korean Society of Propulsion Engineers;2023-04-30
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