Supply Result
| Year | Customer | Equipment Name | Note |
|---|---|---|---|
| 1965 | For the university | Shock Wind Tunnel | Shock wave generating method : Free-Poston-Driven Type Compression Tube Dimensions : 216mm-dia About 8m long Shock Tube Dimensions : 100mm-dia About 10m long Measuring Section : 300mm-dia Mach number : Mach 20 |
| 1997 | For the laboratory and the Agency | High Enthalpy Shock Tunnel(HIEST) | In operation at Kakuda Research Center, National Aerospace Laboratory of Japan |
