Beechcraft T-34 Mentor vs. Lockheed U-2
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Beechcraft T-34 Mentor |
versus |
Lockheed U-2 |
7.92 m |
25 ft 11 in |
length |
19.2 m |
63 ft 0 in |
2.95 m |
9 ft 8 in |
height |
4.8 m |
15 ft 9 in |
10.03 m |
32 ft 11 in |
wingspan |
32 m |
105 ft |
1 x Continental Motors IO-520 engine |
engines |
1 × General Electric F118-101 |
Approximately 300 hp |
thrust per engine |
17,000 lbf (76 kN) |
Approximately 300 hp |
total thrust |
17,000 lbf (76 kN) |
3,100 lb |
1,406 kg |
MTOW |
18,144 kg |
40,000 lb |
1,111 km |
600 nm |
range |
6,090 nm |
11,278 km |
190 mph |
306 km/h |
cruise speed |
475 mph |
764 km/h |
Pilot and one passenger |
capacity |
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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.