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

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

3 Citations (Scopus)

Abstract

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.

Original languageEnglish
Title of host publication15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Publication statusPublished - 2008 Dec 1
Event15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference - Dayton, OH, United States
Duration: 2008 Apr 282008 May 1

Publication series

Name15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Conference

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

ASJC Scopus subject areas

  • Engineering(all)

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