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A rotating detonation rocket engine was designed and studied. The engine utilized a highly reactive propellant combination to provide ignition. Results showed very high detonation wave speeds and several types of detonation behavior.
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This page is a summary of: Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine, Journal of Propulsion and Power, November 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b37666.
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