Pratt & Whitney PW2000

Bypass Ratio

Diameter

1993.9 mm

Length

3728.72 mm

Dry Weight

3220.506 kg

Thrust To Weight

5.41

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 6	Overall Pressure Ratio —	Afterburner No

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Name	Aircraft Engine	Number of Engines	Length (m)	Flat Wing Span (m)	Max Seating
757-200	Pratt & Whitney PW2000	2	47.3	38
Boeing C-17 Globemaster III	Pratt & Whitney PW2000	4	53.0352	51.5112	102
Boeing C-32	Pratt & Whitney PW2000	2	47.244	37.7952

All data (16 fields)

Name: Pratt & Whitney PW2000
Aircraft Engine Manufacturer: Pratt & Whitney
Aircraft Engine Type: Turbofan
Dry Weight (kg): 3220.506
Diameter (mm): 1993.9
Length (mm): 3728.72
Wikipedia Article (URL): en.wikipedia.org/wiki/Pratt_%26_Whitney_PW2000
Fuel: Jet-A, Aviation kerosene
Geared Fan: No
Combustion Chamber: Annular
Afterburner: No
Streams: 2
Bypass Ratio: 6
Thrust To Weight: 5.41
Compressor Description: Axial, 1 stage fan with 36 blades, 4 stage LP, 12 stage HP
Turbine Description: 2 stage HP, 5 stage LP