Lockheed U-2 vs. Short 360

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Lockheed U-2 versus Short 360
19.2 m 63 ft 0 in length 17.74 m 58 ft 2 in
4.8 m 15 ft 9 in height 6.8 m 22 ft 4 in
32 m 105 ft wingspan 22.72 m 74 ft 6 in
1 × General Electric F118-101 engines 2 x Pratt & Whitney Canada PT6A-65R
17,000 lbf (76 kN) thrust per engine 2,430 lbs
17,000 lbf (76 kN) total thrust 4,860 lbs
18,144 kg 40,000 lb MTOW 28,400 lb 12,882 kg
6,090 nm 11,278 km range 820 nm 1,519 km
475 mph 764 km/h cruise speed 220 kts 137 mph
capacity 36
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.