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 language | English |
|---|---|
| Title of host publication | 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014 |
| Publisher | American Institute of Aeronautics and Astronautics Inc. |
| ISBN (Print) | 9781624103032 |
| DOIs | |
| Publication status | Published - 2014 |
| Event | 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 - Cleveland, United States Duration: 2014 Jul 28 → 2014 Jul 30 |
Other
| Other | 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 |
|---|---|
| Country | United States |
| City | Cleveland |
| Period | 14/7/28 → 14/7/30 |
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ASJC Scopus subject areas
- Energy Engineering and Power Technology
- Aerospace Engineering
- Control and Systems Engineering
- Electrical and Electronic Engineering
- Mechanical Engineering
Cite this
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 proceeding › Conference contribution
}
TY - GEN
T1 - Thrust measurement of rotating detonation engine by sled test
AU - Kato, Yuichi
AU - Ishihara, Kazuki
AU - Gawahara, Keita
AU - Matsuoka, Ken
AU - Kasahara, Jiro
AU - Matsuo, Akiko
AU - Funaki, Ikkoh
PY - 2014
Y1 - 2014
N2 - 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.
AB - 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.
UR - http://www.scopus.com/inward/record.url?scp=84913529370&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84913529370&partnerID=8YFLogxK
U2 - 10.2514/6.2014-4034
DO - 10.2514/6.2014-4034
M3 - Conference contribution
AN - SCOPUS:84913529370
SN - 9781624103032
BT - 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
PB - American Institute of Aeronautics and Astronautics Inc.
ER -