Utilized including for the acquisition of aerodynamic characteristics when taking off or landing an aircraft or when in low speed flight

| Department | Aviation Technology Directorate |
|---|---|
| Specifications | Type: Continuous circulation type Test section measurement: 2 m × 2 m square cross section, length of 4m Low-speed wind tunnel performance: Regular use in the range of 3 to 60 m/s (continuous), maximum of 67 m/s Gust generator: Robot model support system: High-pressure air source facility: |
| Year of completion | FY 1971 |
Fees |
194,489 yen/day (Current as of April 1, 2026) *The usage fee above includes the general management fee. |