Status report of JAXA Combined-cycle Engine research program in 2008
- Paper number
IAC-08.D2.5.7
- Author
Mr. Tetsuo Hiraiwa, Japan Aerospace Exploration Agency (JAXA), Japan
- Coauthor
Dr. Katsuhiro ITO, Japan Aerospace Exploration Agency (JAXA), Japan
- Coauthor
Dr. Takeshi Kanda, Japan Aerospace Exploration Agency (JAXA), Japan
- Coauthor
Dr. Sadatake Tomioka, Japan Aerospace Exploration Agency (JAXA), Japan
- Coauthor
Mr. Kouichiro TANI, Japan Aerospace Exploration Agency (JAXA), Japan
- Coauthor
Mr. Shuichi UEDA, Japan
- Year
2008
- Abstract
In 2008, JAXA will conduct several, new experimental trials for the combined-cycle engine as a future space transportation propulsion system. In late 2007, a flight test project started. A prototype model for the flight test will soon be tested at the ground test facility for CAMUI sounding rocket system. HIEST, the world largest shock tube, will take a part in the fundamental experimental research work for the combustor. This paper also presents recent results of ground tests with the modified combined-cycle engine.
- Abstract document
- Manuscript document
IAC-08.D2.5.7.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.