Hypersonic turbojet engine design of a balloon-based flight testing vehicle

Hiroaki Kobayashi*, Shujiro Sawai, Hideyuki Taguchi, Takayuki Kojima, Katsuyoshi Fukiba, Kazuhisa Fujita, Tetsuya Sato

*この研究の対応する著者

研究成果: Conference contribution

3 被引用数 (Scopus)

抄録

JAXA is developing Mach 5 hypersonic turbojet engine technology that can be applied in a future hypersonic transport. Now, in Jet Engine Technology Research Center of JAXA, the experimental study, which uses a 1/10 scale-model engine, is conducted. In parallel to engine development activities, a new supersonic flight-testing vehicle for the hypersonic turbojet engine is under development since 2004. In this paper, the system configuration of the flight-testing vehicle is outlined and development status is reported.

本文言語English
ホスト出版物のタイトル15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
出版ステータスPublished - 2008 12月 1
イベント15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference - Dayton, OH, United States
継続期間: 2008 4月 282008 5月 1

出版物シリーズ

名前15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Conference

Conference15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
国/地域United States
CityDayton, OH
Period08/4/2808/5/1

ASJC Scopus subject areas

  • 工学(全般)

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