Lockheed U-2 vs. Praetor 600
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Lockheed U-2 |
versus |
Praetor 600 |
19.2 m |
63 ft 0 in |
length |
17.02 m |
55 ft 10 in |
4.8 m |
15 ft 9 in |
height |
6.2 m |
20 ft 4 in |
32 m |
105 ft |
wingspan |
20.97 m |
68 ft 9 in |
1 × General Electric F118-101 |
engines |
2 Honeywell HTF7500E |
17,000 lbf (76 kN) |
thrust per engine |
7,036 lbf |
17,000 lbf (76 kN) |
total thrust |
14,072 lbf |
18,144 kg |
40,000 lb |
MTOW |
31,750 lb |
14,397 kg |
6,090 nm |
11,278 km |
range |
4,018 nm |
7,435 km |
475 mph |
764 km/h |
cruise speed |
466 kts |
290 mph |
|
capacity |
12 |
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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.