IDEAL THERMODYNAMIC PERFORMANCE RESULTS FOR ROTATING DETONATION ROCKET ENGINE THRUST CHAMBERS USING CEA

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Veröffentlicht in:AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Pressure gain combustion
1. Verfasser: Paulson, Eric J. (VerfasserIn)
Weitere Verfasser: Kimura, Randon (VerfasserIn), Hargus, William A. (VerfasserIn), Sankaran, Venke (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2020
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