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>XF9-1 jet engine >IHI XF9-1 jet engine June 29, 2018 >IHI XF9-1 Japan made prototype jet engine >Delivered IHI XF9-1 jet engine to Japan's Defense Agency Technical Research and Development Institute. >Fan Diameter: 1.0 meter (39 inch) Length: 4.8 meter (189 inch) >normal dry thrust : 11 ton (24,200lbf) >with afterburner thrust : 15 ton (33,000lbf) >Compressor: Twin spool, axial flow augmented turbofan >Compressor: Low aspect ratio 3-stage low-pressure, 6-stage high-pressure compressor >Turbine : Counter-rotating 1-stage high-pressure, 1-stage low-pressure turbines >Turbine : Turbine inlet temperature (TIT) 3272°F (1800 ℃)