Back to Search Start Over

Development study of a precooled turbojet engine

Authors :
Sato, Tetsuya
Taguchi, Hideyuki
Kobayashi, Hiroaki
Kojima, Takayuki
Fukiba, Katsuyoshi
Okai, Daisaku Masaki, Keiichi
Fujita, Kazuhisa
Hongo, Motoyuki
Sawai, Shujiro
Source :
Acta Astronautica. Apr2010, Vol. 66 Issue 7/8, p1169-1176. 8p.
Publication Year :
2010

Abstract

Abstract: A precooled turbojet engine has been developed by JAXA used for the hypersonic airplane and spaceplane. The subscale engine named “S-engine” whose thrust and weight are about 1.2kN and 100kg was designed, fabricated and tested. The components and the system firing tests under the sea-level-static condition were successfully conducted.In the next phase, a flight test of the S-engine is planned using a stratospheric balloon in 2010 called balloon-based operation vehicle (BOV). The vehicle is dropped from an altitude of 40km by a high altitude balloon. After 40s free-fall, the vehicle is pulled up and the S-engine operates for 30s at about Mach 2. High-altitude tests of the core-engine verified the performance and healthiness of the engine under the condition corresponding to the BOV flight trajectory. [Copyright &y& Elsevier]

Details

Language :
English
ISSN :
00945765
Volume :
66
Issue :
7/8
Database :
Academic Search Index
Journal :
Acta Astronautica
Publication Type :
Academic Journal
Accession number :
47824387
Full Text :
https://doi.org/10.1016/j.actaastro.2009.10.006