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Methane is widely discussed as a fuel for reusable rocket engines. We analyzed this cryogenic methane in cooling channels of a subscale rocket combustion chamber and show tha effects close to the critical point are a severe drawback of this fluid.
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This page is a summary of: Experimental Study of Methane Heat Transfer Deterioration in a Subscale Combustion Chamber, Journal of Propulsion and Power, July 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37394.
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