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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.