Bombardier CRJ1000 vs. McDonnell Douglas A-4 Skyhawk

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Bombardier CRJ1000 versus McDonnell Douglas A-4 Skyhawk
39.1 m 128 ft 5 in length 12.19 m 40 ft 0 in
7.5 m 24 ft 7 in height 4.57 m 15 ft
26.2 m 86 ft wingspan 8.08 m 26 ft 6 in
2 GE CF34-8C5A1 turbofans engines 1x Pratt & Whitney J52-P-6A Jet
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 8,500 pound-force
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 8,500 pound-force
41,640 kg 91,800 lb MTOW 11,113 kg 24,500 lb
3,004 km 1,623 nm range 3,222 km 1,739 nm
515 mph 829 km/h cruise speed 586 kts 364 mph
100 (common) capacity Up to 9,155 pounds of weapons on 5 hardpoints
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.