de Havilland Canada DHC-2 Beaver vs. North American BT-9
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de Havilland Canada DHC-2 Beaver |
versus |
North American BT-9 |
13.56 m |
44 ft 6 in |
length |
8.79 m |
28 ft 10 in |
5 m |
16 ft 5 in |
height |
2.82 m |
9 ft 3 in |
16.56 m |
54 ft 4 in |
wingspan |
10.97 m |
36 ft |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
1 x Wright R-975-3 radial engine |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
Approximately 440 hp |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
Approximately 440 hp |
24,200 lb |
10,977 kg |
MTOW |
4,300 lb |
1,950 kg |
2,535 km |
1,369 nm |
range |
917 km |
495 nm |
228 mph |
367 km/h |
cruise speed |
150 mph |
241 km/h |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
Pilot and one passenger |
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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.