Canadair CT-114 Tutor vs. North American B-25 Mitchell
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Canadair CT-114 Tutor |
versus |
North American B-25 Mitchell |
9.75 m |
32 ft 0 in |
length |
16.15 m |
53 ft 0 in |
2.84 m |
9 ft 4 in |
height |
5 m |
16 ft 4 in |
11.07 m |
36 ft 4 in |
wingspan |
20.58 m |
67 ft 6 in |
1 Orenda J85-CAN-40 turbojet |
engines |
2 x Wright R-2600-92 Twin Cyclone |
2,950 lbs |
thrust per engine |
1,700 horsepower |
2,950 lbs |
total thrust |
3,400 horsepower |
3,331 kg |
7,350 lb |
MTOW |
7,484 kg |
16,500 lb |
1,520 km |
821 nm |
range |
1,350 mi |
1,175 nm |
310 knots |
180 mph |
cruise speed |
233 MPH |
375 km/h |
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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.