Lockheed U-2 vs. Beechcraft T-6 Texan II
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here.
Lockheed U-2 |
versus |
Beechcraft T-6 Texan II |
19.2 m |
63 ft 0 in |
length |
10.18 m |
33 ft 4 in |
4.8 m |
15 ft 9 in |
height |
3.29 m |
10 ft 10 in |
32 m |
105 ft |
wingspan |
10.21 m |
33 ft 6 in |
1 × General Electric F118-101 |
engines |
1 x Pratt & Whitney Canada PT6A-68 |
17,000 lbf (76 kN) |
thrust per engine |
1100 lbs |
17,000 lbf (76 kN) |
total thrust |
1100 lbs |
18,144 kg |
40,000 lb |
MTOW |
6,250 lb |
2,835 kg |
6,090 nm |
11,278 km |
range |
900 nm |
1,667 km |
475 mph |
764 km/h |
cruise speed |
320 kts |
199 mph |
|
capacity |
2 |
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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.