Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine
Author:
Affiliation:
1. Nagoya Daigaku
2. Keio Gijuku Daigaku
3. Uchu Kagaku Kenkyujo
4. Muroran Kogyo Daigaku
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0232
Reference25 articles.
1. Detonative propulsion
2. Pressure History at the Thrust Wall of a Simplified Pulse Detonation Engine
3. Reactive impulse from the explosion of a gas mixture in a semiinfinite space
4. Direct Experimental Impulse Measurements for Detonations and Deflagrations
5. Analytical Model for the Impulse of Single-Cycle Pulse Detonation Tube
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