A Simple Model for Rotating Detonation Rocket Engine Sizing and Performance Estimates
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference23 articles.
1. Numerical investigation of operational performance in a methane-oxygen rotating detonation rocket engine
2. Thermodynamic Cycle Analysis of Pulse Detonation Engines
3. Ideal Thermodynamic Performance Results for Rotating Detonation Rocket Engine Thrust Chambers Using CEA
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Experimental validation of rotating detonation for rocket propulsion;Scientific Reports;2023-08-30
2. Rotating Detonation Combustion for Advanced Liquid Propellant Space Engines;Aerospace;2022-10-07
3. Computational Fluid Dynamic Optimization of an Experimental Rotating Detonation Rocket Engine Nozzle;AIAA AVIATION 2022 Forum;2022-06-20
4. Performance and Business Case Impact Assessment for Launch Systems Utilizing RDRE Propulsion;2022 IEEE Aerospace Conference (AERO);2022-03-05
5. Computational Assessment of Inlet Backflow Effects on Rotating Detonation Engine Performance and Operability;AIAA SCITECH 2022 Forum;2022-01-03
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