Lockheed U-2 vs. Temco TT Pinto

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Lockheed U-2 versus Temco TT Pinto
19.2 m 63 ft 0 in length 9.33 m 30 ft 7 in
4.8 m 15 ft 9 in height 3.3 m 10 ft 10 in
32 m 105 ft wingspan 9.09 m 29 ft 1
1 × General Electric F118-101 engines 1 × Continental YJ69-T-9
17,000 lbf (76 kN) thrust per engine 920 lb f (4.1 kN)
17,000 lbf (76 kN) total thrust 920 lb f (4.1 kN)
18,144 kg 40,000 lb MTOW 4,453 lb 2,020 kg
6,090 nm 11,278 km range 300 km 162 nm
475 mph 764 km/h cruise speed 345 mph 555 km/h
capacity Fuel capacity: 119 US gal (99 imp gal; 450 L) normal; 165 US gal (137 imp gal; 620 L) max
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.