Precooled turbojet engine flight experiment using balloon-based operation vehicle-Reference-Cited by-同舟云学术

Precooled turbojet engine flight experiment using balloon-based operation vehicle

Published:2006-07 Issue:1-5 Volume:59 Page:263-270
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Fujita K.,Sawai S.,Kobayashi H.,Tsuboi N.,Taguchi H.,Kojima T.,Okai K.,Sato T.,Miyaji Koji

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference8 articles.

1. S. Sawai, H. Kobayashi, K. Fujita, T. Sato, N. Tanatsugu, Conceptual study on concise flight test for development of space plane powered by air breathing engine, IAC-04.V.8.05, 55th International Astronautical Congress, Vancouver, Canada, 2004.

2. Development study on air turbo ramjet for a future space plane;Tanatsugu;Journal of Space Technology and Science,1993

3. H. Kobayashi, T. Sato, H. Taguchi, K. Fujita, S. Sawai, N. Tanatsugu, T. Kojima, K. Okai, Y. Maru, Development status of Mach 6 turbojet engine in JAXA, IAC-04-S.5.04, 55th International Astronautical Congress, Vancouver, Canada, 2004.

4. Development study of Mach 6 turbojet engine with air-precooling;Sato;Journal of the British Interplanetary Society,2005

5. H. Taguchi, T. Sato, H. Kobayashi, T. Kojima, K. Okai, K. Fujita, Design study on a small pre-cooled turbojet engine for flight experiment, AIAA Paper 2005-3419, 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy, May 2005.

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