Auster AOP.9 vs. Lockheed U-2

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Auster AOP.9 versus Lockheed U-2
7.23 m 23 ft 9 in length 19.2 m 63 ft 0 in
2.72 m 8 ft 11 in height 4.8 m 15 ft 9 in
11.1 m 36 ft 5 in wingspan 32 m 105 ft
1 x Blackburn Cirrus Bombardier 203 engines 1 × General Electric F118-101
134 kW (180 hp) thrust per engine 17,000 lbf (76 kN)
134 kW (180 hp) (As it has only one engine) total thrust 17,000 lbf (76 kN)
966 kg 2,130 lb MTOW 18,144 kg 40,000 lb
628 km 339 nm range 6,090 nm 11,278 km
177 km/h 110 mph cruise speed 475 mph 764 km/h
3 (pilot and two passengers) 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.