Conceptual Study on hypersonic airplanes using pre-cooled turbojet

Hideyuki Taguchi, Akira Murakami, Tetsuya Sato, Takeshi Tsuchiya

研究成果: Conference contribution

8 被引用数 (Scopus)

抄録

Conceptual Study on hypersonic airplanes with Mach 5 cruising capability is performed in order to improve the speed of intercontinental air transportations. Requirements for engine performance, thrust to mass ratio and heat resistant structure are discussed. As a result, reference concept of a hypersonic airplane with pre-cooled turbojet engine with liquid hydrogen fuel is shown. Then, a small hypersonic flight experiment is planned for demonstration of Mach 5 cruising technologies. Aerodynamic shape of the experimental vehicle is examined by CFD and wind tunnel tests.

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 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 282008 5 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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