The HSWT is a tri-sonic, blow down tunnel with a Mach number range of 0.3 to 4.8. The test section measures 4’ X 4’ X 6’ for transonic testing and 4’ X 4’ X 5’ for supersonic testing.
View in Google Earth Categories: Scientific - Test Facility, Safari Submissions
Links: www.lockheedmartin.com
By: Mike1989

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