The tunnel has an octagonal test section with diagonal distance of 1.75 meters. The maximum speed is 35 m/s (120km/h). Six-components balance and smoke generation facilities enable us to examine aerodynamics and flow around aerospace vehicles.

Super-sonic wind tunnel facility "The tunnel has a rectangular test section whose cross section is 100 x150mm. The maximum Mach number through the test section is 1.6. Flow around models can be visualized by Schlieren optics."

Microstructural observation of various materials using a scanning electron microscope.

Rocket engine and gas turbine can be operated. Experimental research on Hybrid rocket engines is conducted. A micro gas turbine is operated in the undergraduate course experiment.