Detonation engine development for reaction control systems of a spacecraft

Keita Gawahara, Hisahiro Nakayama, Jiro Kasahara, Ken Matsuoka, Sadatake Tomioka, Tetsuo Hiraiwa, Akiko Matsuo, Ikkoh Funaki

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

1 Citation (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 and simple structure. Taking this advantage of its benefits, application to the reaction control system of a spacecraft is expected. Toward the practical use, the knowledge of the detonation propagation in operation and quantification of stable operating range is essential. In the present study, we have produced the RDE with the linear channel that specializes in visualization. The first experimental results of this RDE are reported. The main purpose is obtaining basic combustion characteristics. The optical access of the RDE can be easy by linear channel. In the experiment, the propagation of the detonation wave front is confirmed by a high speed video camera and pressure sensors. The location information of the wave front obtained from the image, the x-t diagram after ignition was obtained. Thereby, the transition to detonation is confirmed. The propagation of the multi-wave front in the steady state was confirmed by the images and pressure sensor. Propagation velocity of the wave front is also obtained by the pressure history and the images.

Original languageEnglish
Title of host publication49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624102226
DOIs
Publication statusPublished - 2013 Jan 1
Event49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013 - San Jose, United States
Duration: 2013 Jul 142013 Jul 17

Publication series

Name49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Volume1 PartF

Conference

Conference49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, JPC 2013
CountryUnited States
CitySan Jose
Period13/7/1413/7/17

ASJC Scopus subject areas

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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  • Cite this

    Gawahara, K., Nakayama, H., Kasahara, J., Matsuoka, K., Tomioka, S., Hiraiwa, T., Matsuo, A., & Funaki, I. (2013). Detonation engine development for reaction control systems of a spacecraft. In 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference; Vol. 1 PartF). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2013-3721