Detonation engine development for reaction control systems of a spacecraft
Author:
Affiliation:
1. University of Tsukuba
2. Japan Aerospace Exploration Agency (JAXA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3721
Reference9 articles.
1. Intermittent Detonation as a Thrust-Producing Mechanism
2. Numerical Investigation of Rotating Detonation Engines
3. Airbreathing Rotating Detonation Wave Engine Cycle Analysis
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