Bombardier CRJ1000 vs. Lockheed Martin C-130J Super Hercules

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Bombardier CRJ1000 versus Lockheed Martin C-130J Super Hercules
39.1 m 128 ft 5 in length 34.37 m 112 ft 9 in
7.5 m 24 ft 7 in height 11.86 m 38 ft 11 in
26.2 m 86 ft wingspan 40.41 m 132 ft 7 in
2 GE CF34-8C5A1 turbofans engines 4 x Rolls-Royce AE 2100D3 turboprop engines
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine Approximately 4,700 hp per engine
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust Approximately 18,800 hp total
41,640 kg 91,800 lb MTOW 76,610 kg 168,900 lb
3,004 km 1,623 nm range 4,600 km 2,485 nm
515 mph 829 km/h cruise speed 660 km/h 410 mph
100 (common) 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.