BAC Jet Provost vs. Lockheed Martin F-35 Lightning II

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BAC Jet Provost versus Lockheed Martin F-35 Lightning II
10.36 m 34 ft 0 in length 15.67 m 51 ft 4 in
3.1 m 10 ft 2 in height 4.33 m 14 ft 2 in
11.25 m 36 ft 11 in wingspan 10.7 m 35 ft 1 in
1 x Bristol Siddeley Viper 201 engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
2,500 lb = 1,134 kg thrust per engine 40,000 lb
2,500 lb = 1,134 kg total thrust 40,000 lb
4,173 kg 9,200 lb MTOW 31,800 kg 70,000 lb
1,448 km 782 nm range 1,380 mi 1,200 nm
440 mph 708 km/h 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.