SLS_TDT: Mike Ramsey, Martin Sekula, and David Piatak in the control room of the Transonic Dynamic Tunnel testing the Space Launching System model. Engineers, Martin Sekula, David Piatak and Mike Ramsey
NASA
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Mach Number: Up to 1.2
Reynolds Number: 0.30 – 10.0 x 106 per foot
Test Gases: Air or R-134a
Test Section Size: 16 ft by 16 ft
Length: 8 feet
Transonic Dynamics Tunnel Fact Sheet
