Thrust Validation of Rotating Detonation Engine System by Moving Rocket Sled Test-Reference-Cited by-同舟云学术

Thrust Validation of Rotating Detonation Engine System by Moving Rocket Sled Test

Published:2021-05 Issue:3 Volume:37 Page:419-425
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Goto Keisuke,Kato Yuichi,Ishihara Kazuki,Matsuoka Ken,Kasahara Jiro,Matsuo Akiko¹,Funaki Ikkoh²,Nakata Daisuke,Higashino Kazuyuki,Tanatsugu Nobuhiro

Affiliation:

1. Keio University, Yokohama, Kanagawa 223-8522, Japan

2. Japan Aerospace Exploration Agency (JAXA), Sagamihara, Kanagawa 252-5210, Japan

Funder

Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

Japan Society for the Promotion of Science

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference28 articles.

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3. Detonative propulsion

4. LiJ. M.TeoC. J.KhooB. C.YaoS.WangC. (eds.), Detonation Control for Propulsion Pulse Detonation and Rotating Detonation Engines, Springer International, Cham, Switzerland, 2018, pp. 1–235. 10.1007/978-3-319-68906-7

5. Rotating Detonation Wave Propulsion: Experimental Challenges, Modeling, and Engine Concepts

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