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We propose a new theoretical tradeoff framework that maximizes the specific impulse as the engine performance and the cooling liquid film length as the cooling performance, which leads to the optimal architecture of liquid rocket engine.

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This page is a summary of: Optimal Liquid Engine Architecture by Performance-Cooling Tradeoff Analysis, Journal of Propulsion and Power, March 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b39409.
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