Research Resource code：5000002713
Update date：Nov. 01, 2004
1m×1m Supersonic Wind Tunnel
Experience equipment, Facilities, etc
Main Objectives: To study aerodynamics in supersonic
User environment and conditions：
flight and to research and develop the supersonic
transport and supersonic projectile.
Performance: Test Section 1m×1m
Duration more than 40 seconds.
Mach Number 1.4~4.0 Compressor,
Air Compressor common use with the transonic wind tunnel.
Completion Year: FY 1961.
Use: To study aerodynamics in supersonic flight and to
research and develop the supersonic transport and
Instruments on models, sensor/data transfer are to be prepared by a user as a rule
User procedures and method：
Refer to Web Page of JAXA
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