Lockheed U-2 vs. Bell 412
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Lockheed U-2 |
versus |
Bell 412 |
19.2 m |
63 ft 0 in |
length |
17,10 m |
56 ft 1 in |
4.8 m |
15 ft 9 in |
height |
3,48 m |
11 ft 5 in |
32 m |
105 ft |
wingspan |
|
|
1 × General Electric F118-101 |
engines |
2 x Pratt & Whitney Canada PT6T-3D turboshaft engines |
17,000 lbf (76 kN) |
thrust per engine |
1,800 hp |
17,000 lbf (76 kN) |
total thrust |
3,600 hp |
18,144 kg |
40,000 lb |
MTOW |
5,400 kg |
11,905 lb |
6,090 nm |
11,278 km |
range |
659 km |
356 nm |
475 mph |
764 km/h |
cruise speed |
259 km/h |
161 mph |
|
capacity |
13 |
|
|
rotor diameter |
14.0 m |
45 ft 11 in |
|
|
rate of climb |
9.5 m/s |
1,870 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.