de Havilland DH-82 Tiger Moth vs. Lockheed Martin F-35 Lightning II

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de Havilland DH-82 Tiger Moth versus Lockheed Martin F-35 Lightning II
7.29 m 23 ft 11 in length 15.67 m 51 ft 4 in
2.67 m 8 ft 9 in height 4.33 m 14 ft 2 in
8.97 m 29 ft 5 in wingspan 10.7 m 35 ft 1 in
1 x de Havilland Gipsy Major I inline engine engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
Approximately 130 hp thrust per engine 40,000 lb
Approximately 130 hp total thrust 40,000 lb
1,825 lb 828 kg MTOW 31,800 kg 70,000 lb
322 km 174 nm range 1,380 mi 1,200 nm
78 mph 126 km/h cruise speed 520 kt 302 mph
Pilot and one passenger 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.