Lockheed U-2 vs. Dornier 228

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Lockheed U-2 versus Dornier 228
19.2 m 63 ft 0 in length 16.56 m 54 ft 4 in
4.8 m 15 ft 9 in height 4.86 m 15 ft 11 in
32 m 105 ft wingspan 16.97 m 55 ft 8 in
1 × General Electric F118-101 engines 2 x Garrett TPE331 turboprop engines
17,000 lbf (76 kN) thrust per engine Approximately 776 kW per engine
17,000 lbf (76 kN) total thrust Approximately 1,552 kW total
18,144 kg 40,000 lb MTOW 5,650 kg 12,456 lb
6,090 nm 11,278 km range 1,465 km 791 nm
475 mph 764 km/h cruise speed 350 km/h 217 mph
capacity Up to 19 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.