de Havilland Canada DHC-2 Beaver vs. Lockheed U-2
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de Havilland Canada DHC-2 Beaver |
versus |
Lockheed U-2 |
13.56 m |
44 ft 6 in |
length |
19.2 m |
63 ft 0 in |
5 m |
16 ft 5 in |
height |
4.8 m |
15 ft 9 in |
16.56 m |
54 ft 4 in |
wingspan |
32 m |
105 ft |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
1 × General Electric F118-101 |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
17,000 lbf (76 kN) |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
17,000 lbf (76 kN) |
24,200 lb |
10,977 kg |
MTOW |
18,144 kg |
40,000 lb |
2,535 km |
1,369 nm |
range |
6,090 nm |
11,278 km |
228 mph |
367 km/h |
cruise speed |
475 mph |
764 km/h |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
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.