IHI Corporation XF5

Maximum Takeoff Thrust

49 kN

Diameter

610 mm

Length

3000 mm

Dry Weight

644 kg

Thrust To Weight

7.8

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 —	Overall Pressure Ratio —	Afterburner Yes

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Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
Klimov RD-33	Klimov	50	0.49		Compare
Snecma M88	SNECMA	50	0.3		Compare
SPEY Mk511	Rolls-Royce	50.7	0.64	19.9	Compare
Tumansky R-21	Tumansky	46.1			Compare
Lyulka AL-5	Lyulka-Saturn	52			Compare
Pratt & Whitney J57	Pratt & Whitney	52			Compare

All data (16 fields)

Name: IHI Corporation XF5
Aircraft Engine Manufacturer: IHI Corporation
Aircraft Engine Type: Turbofan
Dry Weight (kg): 644
Diameter (mm): 610
Length (mm): 3000
Wikipedia Article (URL): en.wikipedia.org/wiki/IHI_Corporation_XF5
Geared Fan: No
Combustion Chamber: annular
Afterburner: Yes
Streams: 2
Maximum Takeoff Thrust (kN): 49
Thrust To Weight: 7.8
Afterburner Thrust (kN): 49
Compressor Description: axial, 3 stage fan, 6 compressor stage
Turbine Description: 1 stage high pressure turbine, 1 stage low pressure turbine