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Pratt & Whitney Engines
F100-PW-220/F100-PW-220E TUBOFAN ENGINE
Aircraft using this engine (click
here)
Aircraft using this engine (click here)
Engine Characteristic |
|
Maximum Thrust (Full Augmentation) | 23,770 pounds (105.7 kN) |
Intermediate Thrust (Nonaugmented) | 14,590 pounds (64.9 kN) |
Weight | 3,2324 pounds (1467 kg) |
Length | 191 in. (4.85 m) |
Inlet Diameter | 34.8 in. (0.88 m) |
Maximum Diameter | 46.5 in. (1. 18 in) |
Bypass Ratio | 0.6 |
Overall Pressure Ratio | 25 to 1 |
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Funded in part by | Used with permission from Pratt & Whitney |
Updated: February 23, 1999