Bombardier CRJ1000 vs. Mitsubishi A6M Zero

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Bombardier CRJ1000 versus Mitsubishi A6M Zero
39.1 m 128 ft 5 in length 9.06 m 29 ft 9 in
7.5 m 24 ft 7 in height 3.05 m 10 ft
26.2 m 86 ft wingspan 12 m 39 ft 4 in
2 GE CF34-8C5A1 turbofans engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
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 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
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 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
41,640 kg 91,800 lb MTOW 2,800 kg 6,170 lb
3,004 km 1,623 nm range 1,010 nm 1,871 km
515 mph 829 km/h cruise speed 180 knots 105 mph
100 (common) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.