BAC Jet Provost vs. Lockheed Martin C-130J Super Hercules

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BAC Jet Provost versus Lockheed Martin C-130J Super Hercules
10.36 m 34 ft 0 in length 34.37 m 112 ft 9 in
3.1 m 10 ft 2 in height 11.86 m 38 ft 11 in
11.25 m 36 ft 11 in wingspan 40.41 m 132 ft 7 in
1 x Bristol Siddeley Viper 201 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
2,500 lb = 1,134 kg thrust per engine Approximately 4,700 hp per engine
2,500 lb = 1,134 kg total thrust Approximately 18,800 hp total
4,173 kg 9,200 lb MTOW 76,610 kg 168,900 lb
1,448 km 782 nm range 4,600 km 2,485 nm
440 mph 708 km/h cruise speed 660 km/h 410 mph
capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.