Lockheed U-2 vs. Bell 412

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Lockheed U-2 versus Bell 412
19.2 m 63 ft 0 in length 17,10 m 56 ft 1 in
4.8 m 15 ft 9 in height 3,48 m 11 ft 5 in
32 m 105 ft wingspan
1 × General Electric F118-101 engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
17,000 lbf (76 kN) thrust per engine 1,800 hp
17,000 lbf (76 kN) total thrust 3,600 hp
18,144 kg 40,000 lb MTOW 5,400 kg 11,905 lb
6,090 nm 11,278 km range 659 km 356 nm
475 mph 764 km/h cruise speed 259 km/h 161 mph
capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.