Ishikawajima-Harima F3

Bypass Ratio

0.9

Diameter

635 mm

Length

2006.6 mm

Dry Weight

340.1943 kg

Thrust To Weight

4.9

Specific Fuel Consumption

19.827 g/(kN·s)

Architecture

Fan	Fan Stages —	Fan Blades —	Fan Technology —	Fan Pressure Ratio —
Gearbox	Geared Fan No	Gear —	Reduction Ratio —
LP compressor	Low-Pressure Compressor Stages —	Low-Pressure Compressor Technology —	BP Compressor Pressure Ratio —
IP compressor	Intermediary-Pressure Compressor Stages —	Intermediary-Pressure Compressor Technology —	IP Compressor Pressure Ratio —
HP compressor	High-Pressure Compressor Stages —	High-Pressure Compressor Technology —	HP Compressor Pressure Ratio —
Combustor	Combustion Chamber annular
HP turbine	High Pressure Compressor Stages —	High-Pressure Turbine Technology —
IP turbine	Intermediary-Pressure Turbine Stages —	Intermediary-Pressure Turbine Technology —
LP turbine	Low-Pressure Turbine Stages —	Low-Pressure Turbine Technology —
Whole engine	Streams 2	Bypass Ratio 0.9	Overall Pressure Ratio —	Afterburner No

No pictures yet for this family.

Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)
Kawasaki T-4	Ishikawajima-Harima F3	2	13	9.94

All data (16 fields)

Name: Ishikawajima-Harima F3
Aircraft Engine Manufacturer: IHI Corporation
Aircraft Engine Type: Turbofan
Dry Weight (kg): 340.1943
Diameter (mm): 635
Length (mm): 2006.6
Wikipedia Article (URL): en.wikipedia.org/wiki/Ishikawajima-Harima_F3
Geared Fan: No
Combustion Chamber: annular
Afterburner: No
Streams: 2
Bypass Ratio: 0.9
Thrust To Weight: 4.9
Specific Fuel Consumption (g/(kN·s)): 19.827
Compressor Description: axial, 2 stage, low pressure compressor, 5 stage high pressure compressor
Turbine Description: single stage high pressure turbine, two stage low pressure turbine