1. A Design Approach of CMC RAM-Combustor Wall;56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2005-10-17
2. Design Study on a Small Pre-Cooled Turbojet Engine for Flight Experiments;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16
3. Hypersonic Ramjet Engine with Balanced Variable Mechanisms;55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2004-10-04
4. Development Status of Mach 6 Turbojet Engine in JAXA;55th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2004-10-04
5. Numerical Analysis of Variable Intake and Nozzle for Hypersonic Engines;12th AIAA International Space Planes and Hypersonic Systems and Technologies;2003-12-15