de Havilland Canada DHC-2 Beaver vs. Scottish Aviation T1 Bulldog
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de Havilland Canada DHC-2 Beaver |
versus |
Scottish Aviation T1 Bulldog |
13.56 m |
44 ft 6 in |
length |
7.11 m |
23 ft 4 in |
5 m |
16 ft 5 in |
height |
2.08 m |
6 ft 10 in |
16.56 m |
54 ft 4 in |
wingspan |
10.21 m |
33 ft 6 in |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
1 x Lycoming O-360-A4M piston engine |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
Approximately 180 hp |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
Approximately 180 hp |
24,200 lb |
10,977 kg |
MTOW |
1,111 kg |
2,450 lb |
2,535 km |
1,369 nm |
range |
1,050 km |
567 nm |
228 mph |
367 km/h |
cruise speed |
222 km/h |
138 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
Instructor pilot and one student |
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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.