Lockheed U-2 vs. Air Tractor AT-802

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Lockheed U-2 versus Air Tractor AT-802
19.2 m 63 ft 0 in length 10.16 m 33 ft 4 in
4.8 m 15 ft 9 in height 3.66 m 12 ft
32 m 105 ft wingspan 18.29 m 60 ft
1 × General Electric F118-101 engines 1 x Pratt & Whitney Canada PT6A-67F turboprop engine
17,000 lbf (76 kN) thrust per engine 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
17,000 lbf (76 kN) total thrust 1,200 to 1,550 shaft horsepower (895 to 1,156 kW)
18,144 kg 40,000 lb MTOW 7,257 kg 16,000 lb
6,090 nm 11,278 km range 1,125 km 607 nm
475 mph 764 km/h cruise speed 240 km/h 149 mph
capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.