J-GLOBAL ID:201110026341062365   Research Resource code:5000002709 Update date:Jan. 12, 2005

1.27m Hypersonic Wind Tunnel System

Owning Organization:
Contact: HAMAMOTO Shigeru
Resource classification: Experience equipment, Facilities, etc
Diameter 127cm Hypersonic Wind Tunnel. Mach Number 10.
Application: To study aerodynamics in hypersonic flight
and to develop the supersonic transports and projectiles.
Construction Date: FY1994.
User environment and conditions:
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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