Study on a Rotary-Valved Four-Cylinder Pulse Detonation Rocket : Thrust Measurement by Ground Test

Author:

Morozumi Tomohito1,Sakamoto Ryuki1,Kashiwazaki Takashi1,Kasahara Jiro2,Matsuoka Ken2,Matsuo Akiko3,Funaki Ikkoh4

Affiliation:

1. University of Tsukuba

2. University of Nagoya

3. Keio University

4. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Cited by 8 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 research on operation performance and acoustic behavior of two-phase dual-tube pulse detonation engine;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-04-26

2. The Experimental Study about the Effect of Operating Conditions on Multi-tube Pulse Detonation Engine Performance;International Journal of Aeronautical and Space Sciences;2018-03

3. Plasma-assisted Rotating Detonation Combustor Operation;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

4. Efforts on High-Frequency Pulse Detonation Engines;Journal of Propulsion and Power;2017-01

5. Numerical Study for Rotating Detonation Propagation in a Two-Parallel-Plane Combustor;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22

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