Flight demonstration of a pulse detonation rocket system todoroki II

Ken Matsuoka, Shunsuke Takagi, Jiro Kasahara, Tomohito Morozumi, Akiko Matsuo, Ikkoh Funaki

研究成果: Conference contribution

抄録

We constructed a rotary-valved four-cylinder pulse detonation rocket system (Todoroki II) for the flight demonstration. The total length and weight of the vehicle were 1910 mm and approximately 32.5 kg with propellant and purge gas, respectively (detonation tube inner diameter and length: 36 mm and 805 mm, respectively). We investigated the thrust performance of Todoroki II and the thrust-to-weight ratio on grand test. A propellant-based specific impulse of 131 s, a time-averaged thrust of 256 N and a thrust-to weight ratio of 0.8 were achieved. The flight test using the newly-developed launch-recovery system was carried out. The system operated perfectly, and we successfully recovered the Todoroki II without damage. It was confirmed that the rolling by rotating the rotary valve and significant vibration by pulse detonation had a low impact on the flight. The stable pulse detonation operation and the detonation engine thrust in real flight condition (6-degree-of-freedom condition) were validated.

元の言語English
ホスト出版物のタイトルProceedings of the International Astronautical Congress, IAC
出版者International Astronautical Federation, IAF
ページ7529-7534
ページ数6
10
ISBN(印刷物)9781634399869
出版物ステータスPublished - 2014
イベント65th International Astronautical Congress 2014: Our World Needs Space, IAC 2014 - Toronto, Canada
継続期間: 2014 9 292014 10 3

Other

Other65th International Astronautical Congress 2014: Our World Needs Space, IAC 2014
Canada
Toronto
期間14/9/2914/10/3

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Detonation
Rockets
detonation
rockets
thrust
Demonstrations
flight
pulses
propellants
Propellants
flight conditions
specific impulse
flight tests
Engine cylinders
engines
vibration
engine
vehicles
degrees of freedom
recovery

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering
  • Astronomy and Astrophysics

これを引用

Matsuoka, K., Takagi, S., Kasahara, J., Morozumi, T., Matsuo, A., & Funaki, I. (2014). Flight demonstration of a pulse detonation rocket system todoroki II. : Proceedings of the International Astronautical Congress, IAC (巻 10, pp. 7529-7534). International Astronautical Federation, IAF.

Flight demonstration of a pulse detonation rocket system todoroki II. / Matsuoka, Ken; Takagi, Shunsuke; Kasahara, Jiro; Morozumi, Tomohito; Matsuo, Akiko; Funaki, Ikkoh.

Proceedings of the International Astronautical Congress, IAC. 巻 10 International Astronautical Federation, IAF, 2014. p. 7529-7534.

研究成果: Conference contribution

Matsuoka, K, Takagi, S, Kasahara, J, Morozumi, T, Matsuo, A & Funaki, I 2014, Flight demonstration of a pulse detonation rocket system todoroki II. : Proceedings of the International Astronautical Congress, IAC. 巻. 10, International Astronautical Federation, IAF, pp. 7529-7534, 65th International Astronautical Congress 2014: Our World Needs Space, IAC 2014, Toronto, Canada, 14/9/29.
Matsuoka K, Takagi S, Kasahara J, Morozumi T, Matsuo A, Funaki I. Flight demonstration of a pulse detonation rocket system todoroki II. : Proceedings of the International Astronautical Congress, IAC. 巻 10. International Astronautical Federation, IAF. 2014. p. 7529-7534
Matsuoka, Ken ; Takagi, Shunsuke ; Kasahara, Jiro ; Morozumi, Tomohito ; Matsuo, Akiko ; Funaki, Ikkoh. / Flight demonstration of a pulse detonation rocket system todoroki II. Proceedings of the International Astronautical Congress, IAC. 巻 10 International Astronautical Federation, IAF, 2014. pp. 7529-7534
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