Auster AOP.6 vs. Lockheed Martin F-35 Lightning II

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Auster AOP.6 versus Lockheed Martin F-35 Lightning II
7.24 m 23 ft 9 in length 15.67 m 51 ft 4 in
2.55 m 8 ft 4 in height 4.33 m 14 ft 2 in
10.97 m 36 ft wingspan 10.7 m 35 ft 1 in
1× de Havilland Gipsy Major 7 inline piston engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
145 hp (108 kW) thrust per engine 40,000 lb
145 hp (108 kW) total thrust 40,000 lb
2,160 lb 980 kg MTOW 31,800 kg 70,000 lb
507 km 274 nm range 1,380 mi 1,200 nm
174 km/h 108 mph cruise speed 520 kt 302 mph
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.