Fairey Gannet vs. Lockheed Martin C-130J Super Hercules

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Fairey Gannet versus Lockheed Martin C-130J Super Hercules
10.87 m 35 ft 8 in length 34.37 m 112 ft 9 in
3.76 m 12 ft 4 in height 11.86 m 38 ft 11 in
13.87 m 45 ft 6 in wingspan 40.41 m 132 ft 7 in
1 x Bristol Pegasus XVIII radial engine engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 690 hp (515 kW) thrust per engine Approximately 4,700 hp per engine
Approximately 690 hp (515 kW) total thrust Approximately 18,800 hp total
7,005 lb 3,178 kg MTOW 76,610 kg 168,900 lb
840 km 454 nm range 4,600 km 2,485 nm
139 mph 224 km/h cruise speed 660 km/h 410 mph
Pilot, Observer, and Air Gunner 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.