Lockheed U-2 vs. Bell 206

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Lockheed U-2 versus Bell 206
19.2 m 63 ft 0 in length 12.11 m 39 ft 9 in
4.8 m 15 ft 9 in height 2.88 m 9 ft 5 in
32 m 105 ft wingspan
1 × General Electric F118-101 engines 1 × Allison 250-C20B
17,000 lbf (76 kN) thrust per engine 420 shp (313 kW)
17,000 lbf (76 kN) total thrust 420 shp (313 kW)
18,144 kg 40,000 lb MTOW 1,451 kg 3,199 lb
6,090 nm 11,278 km range 374 km 202 nm
475 mph 764 km/h cruise speed 222 km/h 138 mph
capacity 1 pilot + 4 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 425 m/min 1,395 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.