Lockheed U-2 vs. North American T-6 Texan
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Lockheed U-2 |
versus |
North American T-6 Texan |
19.2 m |
63 ft 0 in |
length |
9.0 m |
29 ft 6 in |
4.8 m |
15 ft 9 in |
height |
3.56 m |
11 ft 8 in |
32 m |
105 ft |
wingspan |
12.8 m |
42 ft |
1 × General Electric F118-101 |
engines |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
17,000 lbf (76 kN) |
thrust per engine |
Approximately 600 hp |
17,000 lbf (76 kN) |
total thrust |
Approximately 600 hp |
18,144 kg |
40,000 lb |
MTOW |
5,617 lb |
2,548 kg |
6,090 nm |
11,278 km |
range |
1,175 km |
634 nm |
475 mph |
764 km/h |
cruise speed |
145 mph |
233 km/h |
|
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.