Transpiration Cooling Performance in LOX/Methane Liquid-Fuel Rocket Engines
- 1 May 2005
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 42 (3), 476-486
- https://doi.org/10.2514/1.7587
Abstract
No abstract availableKeywords
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