Lockheed U-2 vs. North American Rockwell OV-10 Bronco
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Lockheed U-2 |
versus |
North American Rockwell OV-10 Bronco |
19.2 m |
63 ft 0 in |
length |
12.7 m |
41 ft 7 in |
4.8 m |
15 ft 9 in |
height |
4.62 m |
15 ft 2 in |
32 m |
105 ft |
wingspan |
12.19 m |
40 ft |
1 × General Electric F118-101 |
engines |
2 x Garrett T76-G-420/421 turboprop engines |
17,000 lbf (76 kN) |
thrust per engine |
Approximately 715 hp each |
17,000 lbf (76 kN) |
total thrust |
Approximately 1,430 hp total |
18,144 kg |
40,000 lb |
MTOW |
14,444 lb |
6,553 kg |
6,090 nm |
11,278 km |
range |
1,931 km |
1,043 nm |
475 mph |
764 km/h |
cruise speed |
244 mph |
393 km/h |
|
capacity |
Pilot and observer |
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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.