Auster AOP.9 vs. Lockheed Martin F-35 Lightning II

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Auster AOP.9 versus Lockheed Martin F-35 Lightning II
7.23 m 23 ft 9 in length 15.67 m 51 ft 4 in
2.72 m 8 ft 11 in height 4.33 m 14 ft 2 in
11.1 m 36 ft 5 in wingspan 10.7 m 35 ft 1 in
1 x Blackburn Cirrus Bombardier 203 engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
134 kW (180 hp) thrust per engine 40,000 lb
134 kW (180 hp) (As it has only one engine) total thrust 40,000 lb
966 kg 2,130 lb MTOW 31,800 kg 70,000 lb
628 km 339 nm range 1,380 mi 1,200 nm
177 km/h 110 mph cruise speed 520 kt 302 mph
3 (pilot and two passengers) capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.