The Supersonic Combustion Ramjet (Scramjet) Test Complex includes a direct-connect combustor test facility, two small-scale complete engine test facilities, the Mach 4 Blow-Down Facility, and the 8-Foot High Temperature Tunnel.
4-Foot Supersonic Unitary Plan Wind Tunnel (UPWT) The versatile 4-Foot Supersonic Unitary Plan Wind Tunnel (UPWT) boasts a robust set of measurement tools and testing techniques for an enhanced understanding of complex fluid dynamics, as well as applied aerodynamics research. + Learn More
20-Inch Supersonic Wind Tunnel (SWT) The 20-Inch Supersonic Wind Tunnel (SWT) is a versatile blow-down facility capable of producing supersonic Mach numbers from 1.6 to 5.0 and subsonic Mach numbers from 0.35 to 0.75. + Learn More
at a Glance
Learn about the capabilities of our facilities and decide which facility best meets your needs + View PDF Document