Hypersonic Turbojet Engine Design of a Balloon-Based Flight Testing Vehicle
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
2. Jet Engine Technology Research Center
3. Future Space Transportation Research Center
4. Waseda University, Shinjuku
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2620
Reference4 articles.
1. Powell, T. H., and Glickstein, M. R. "Precooled Turbojet Engine Cycle for High Mach Number Applications," AIAA-88-2946,1988.
2. Test results of the air turbo ramjet for a future space plane
3. Precooled turbojet engine flight experiment using balloon-based operation vehicle
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