Facility

	Core Laboratory Room #409, 1st Building of Institute of Fluid Science
	Refresh Room Avairable for Break and Meeting Space.
	Supercomputers Owned by Institute of Fluid Science Scalar Parallel Computing System SGI UV2000 (Core 1280, 24.5TFLOPS）other 15 machines Vector Parallel Computing System NEC SX-9（Core 16, 1.6TFLOPS）
	Low-Turbulence Wind Tonnel Owned by Institute of Fluid Science Circulation Type Open Mesurement Section (0.81×0.81 m) Flow Velocity 5 - 70 m/s
	Small Low-Turbelence Wind Tonnel Owned by Institute of Fluid Science Circulation Type Open Mesurement Section (0.29×0.29 m) Flow Velocity 5 - 70 m/s
	High-Enthalpy Shock Tonnel（HIEST） Owned by JAXA Kakuda Space Center Max Enthalpy：25 MJ/kg Max Pressure：150 MPa Max Temperature: 10000 K Test Duration：2 msec

Next Generation Space Transportation Systems Laboratory

Our laboratory is collaborating with Next Generation Space Transportation Laboratory, Department of Aerospace Engineering, Tohoku University.

Development of Mars Airplane

Mars Airplane

Space Thermal Fluid Systems Laboratory is developing Mars Airplane by collaborating with Japan Aerospace Explaration Agency (JAXA) and other universities. We are aming at the launch in late 2020's.

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