Lockheed U-2 vs. AgustaWestland AW109

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Lockheed U-2 versus AgustaWestland AW109
19.2 m 63 ft 0 in length 13,04 m 42 ft 9 in
4.8 m 15 ft 9 in height 3,40 m 11 ft 2 in
32 m 105 ft wingspan
1 × General Electric F118-101 engines 2 × Pratt & Whitney Canada PW206C or 2 × Pratt & Whitney Canada PW207C
17,000 lbf (76 kN) thrust per engine 638 shp (476 kW)
17,000 lbf (76 kN) total thrust 1276 shp (952 kW)
18,144 kg 40,000 lb MTOW 3,175 kg 7,000 lb
6,090 nm 11,278 km range 932 km 503 nm
475 mph 764 km/h cruise speed 285 km/h 177 mph
capacity 1 or 2 pilots + up to 7 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 651 m/min 2,136 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.