Performance Validation of a Single-Tube Pulse Detonation Rocket System
Author:
Affiliation:
1. University of Tsukuba, Tsukuba 305-8573, Japan
2. IHI Aerospace Engineering, Tomioka 370-2307, Japan
3. Japan Aerospace Exploration Agency, Chofu 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.37924
Reference32 articles.
1. Intermittent Detonation as a Thrust-Producing Mechanism
2. Review of Propulsion Applications of Detonation Waves
3. Recent Developments in the Research on Pulse Detonation Engines
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