Bombardier CRJ1000 vs. lockheed C-130 hercules

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Bombardier CRJ1000 versus lockheed C-130 hercules
39.1 m 128 ft 5 in length 29.79 m 97 ft 9 in
7.5 m 24 ft 7 in height 11.66 m 38 ft 3 in
26.2 m 86 ft wingspan 40.41 m 132 ft 7 in
2 GE CF34-8C5A1 turbofans engines 4 x Allison T56-A-15 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 4,590 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 18,360 hp total
41,640 kg 91,800 lb MTOW 70,307 kg 155,000 lb
3,004 km 1,623 nm range 3,760 km 2,031 nm
515 mph 829 km/h cruise speed 540 km/h 335 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.