Auster AOP.9 vs. Lockheed Martin C-130J Super Hercules

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Auster AOP.9 versus Lockheed Martin C-130J Super Hercules
7.23 m 23 ft 9 in length 34.37 m 112 ft 9 in
2.72 m 8 ft 11 in height 11.86 m 38 ft 11 in
11.1 m 36 ft 5 in wingspan 40.41 m 132 ft 7 in
1 x Blackburn Cirrus Bombardier 203 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
134 kW (180 hp) thrust per engine Approximately 4,700 hp per engine
134 kW (180 hp) (As it has only one engine) total thrust Approximately 18,800 hp total
966 kg 2,130 lb MTOW 76,610 kg 168,900 lb
628 km 339 nm range 4,600 km 2,485 nm
177 km/h 110 mph cruise speed 660 km/h 410 mph
3 (pilot and two passengers) 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.