1 min read
Preparations for Next Moonwalk Simulations Underway (and Underwater)
Home
Characteristics
The Flight Dynamics Research Facility (FDRF) is a large, subsonic wind tunnel with a vertical test section for conducting flight dynamics research for stability, controllability, free-fall and aircraft spin, and spin recovery testing of atmospheric vehicles.
Characteristics
- Test Section Dimensions: 20 ft. diam. by 24 ft. high
- Speed: 0 – 172 ft/s (0 – 117 mph)
- Dynamic Pressure: (0 – 35 psf)
- Reynolds Number: 0 – 1.10×10^6 per ft.
- Pressure: Atmospheric
- Temperature: Actively cooled (79° F)
- Test Gas: Air
- Facility Height: 131 ft.
Flight Dynamics Flight Research
Aerosciences Evaluation and Test Capabilities
Explore More
Share
Related Terms
NA
Source
This article was originally published by NASA Breaking News and written by Lillian Gipson.
Read original article on NASA Breaking News