TY - GEN
T1 - Hypersonic turbojet engine design of a balloon-based flight testing vehicle
AU - Kobayashi, Hiroaki
AU - Sawai, Shujiro
AU - Taguchi, Hideyuki
AU - Kojima, Takayuki
AU - Fukiba, Katsuyoshi
AU - Fujita, Kazuhisa
AU - Sato, Tetsuya
PY - 2008/12/1
Y1 - 2008/12/1
N2 - 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.
AB - 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.
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UR - http://www.scopus.com/inward/citedby.url?scp=77958485004&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:77958485004
SN - 9781563479601
T3 - 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
BT - 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
T2 - 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Y2 - 28 April 2008 through 1 May 2008
ER -