Thrust measurement of rotating detonation engine by sled test

Yuichi Kato, Kazuki Ishihara, Keita Gawahara, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Citations (Scopus)

Abstract

Study of a Rotating Detonation Engine (RDE) has been carried out in many research institutions. The RDE has the advantage of high efficiency, simple structure and only once ignition. Toward the practical use for rocket engine, the evaluation of thrust efficiency and the knowledge of combustion under high acceleration or multiple degrees of freedom are essential. In this study, C2H4 + O2 mixture was used as propellant. A Slide mechanism for thrust measyrement was developed, and the mechanism reduced noise and exhausted burned gas. So, the thrust history was acquired and the thrust performance was assessed.

Original languageEnglish
Title of host publication50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624103032
DOIs
Publication statusPublished - 2014
Event50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 - Cleveland, United States
Duration: 2014 Jul 282014 Jul 30

Other

Other50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014
CountryUnited States
CityCleveland
Period14/7/2814/7/30

Fingerprint

Detonation
Engines
Rocket engines
Degrees of freedom (mechanics)
Propellants
Ignition
Gases

ASJC Scopus subject areas

  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

Cite this

Kato, Y., Ishihara, K., Gawahara, K., Matsuoka, K., Kasahara, J., Matsuo, A., & Funaki, I. (2014). Thrust measurement of rotating detonation engine by sled test. In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014 American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2014-4034

Thrust measurement of rotating detonation engine by sled test. / Kato, Yuichi; Ishihara, Kazuki; Gawahara, Keita; Matsuoka, Ken; Kasahara, Jiro; Matsuo, Akiko; Funaki, Ikkoh.

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc., 2014.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Kato, Y, Ishihara, K, Gawahara, K, Matsuoka, K, Kasahara, J, Matsuo, A & Funaki, I 2014, Thrust measurement of rotating detonation engine by sled test. in 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc., 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Cleveland, United States, 14/7/28. https://doi.org/10.2514/6.2014-4034
Kato Y, Ishihara K, Gawahara K, Matsuoka K, Kasahara J, Matsuo A et al. Thrust measurement of rotating detonation engine by sled test. In 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc. 2014 https://doi.org/10.2514/6.2014-4034
Kato, Yuichi ; Ishihara, Kazuki ; Gawahara, Keita ; Matsuoka, Ken ; Kasahara, Jiro ; Matsuo, Akiko ; Funaki, Ikkoh. / Thrust measurement of rotating detonation engine by sled test. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc., 2014.
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