Supply Result
| Year | Customer | Equipment | Remarks (specifications) |
|---|---|---|---|
| 1963 | For the university | 20cm Hypersonic Wind Tunnel | Type : Heating Blow-down Type Measuring Section : φ 200mm Mach Number Irregular : 7, 8, and 9 Total Pressure : 4.9MPa Total Temperature : 600°C |
| 1964 | For the laboratory | Hypersonic Wind Tunnel | Type : Heating Blow-down Type Measuring Section : φ 500mm Mach Number : 5,7,9 and 11(selectable) Total Pressure : 9.8MPa Total Temperature : 1,000°C |
| 1966 | For the university | Hyper-speed Aerodynamic Experimental Facility | Type : Blow-down Type Measuring Section : 150×150mm Mach Number : 2 to 5 Stagnation Temperature : 600°C Duration Time : 5 minutes |
|
1995 |
For the laboratory | Upsized Hypersonic Wind Tunnel (Large Hypersonic Wind Tunnel) | Type : Blow-out with Vacuum Suction Intermittent Type Mach Number : 10 Nozzle Outlet Diameter : φ 1,270mm Total Pressure : 1 to 9.9 MPa Total Temperature : 1073K5 Blowing Time : Vacuum Tank Capacity:2,300m3 20 seconds or more in use Compressed Air source : 18m3 × 2 Units (alternately used) × max. 19.7 MPa Heater : Alumina-pebble Heat Accumulator Type Vacuum Tank : 1150m3 × 2units + 2300m3 × 1unit |
