Lockheed U-2 vs. Meyers OTW
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Lockheed U-2 |
versus |
Meyers OTW |
19.2 m |
63 ft 0 in |
length |
6.71 m |
22 ft 0 in |
4.8 m |
15 ft 9 in |
height |
2.44 m |
8 ft |
32 m |
105 ft |
wingspan |
9.3 m |
30 ft 6 in |
1 × General Electric F118-101 |
engines |
1 x Kinner R-540 radial engine |
17,000 lbf (76 kN) |
thrust per engine |
Approximately 160 hp |
17,000 lbf (76 kN) |
total thrust |
Approximately 160 hp |
18,144 kg |
40,000 lb |
MTOW |
1,575 lb |
715 kg |
6,090 nm |
11,278 km |
range |
603 km |
326 nm |
475 mph |
764 km/h |
cruise speed |
95 mph |
153 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.