Lockheed U-2 vs. North American BT-9
... or view the full comparison list
here.
Lockheed U-2 |
versus |
North American BT-9 |
19.2 m |
63 ft 0 in |
length |
8.79 m |
28 ft 10 in |
4.8 m |
15 ft 9 in |
height |
2.82 m |
9 ft 3 in |
32 m |
105 ft |
wingspan |
10.97 m |
36 ft |
1 × General Electric F118-101 |
engines |
1 x Wright R-975-3 radial engine |
17,000 lbf (76 kN) |
thrust per engine |
Approximately 440 hp |
17,000 lbf (76 kN) |
total thrust |
Approximately 440 hp |
18,144 kg |
40,000 lb |
MTOW |
4,300 lb |
1,950 kg |
6,090 nm |
11,278 km |
range |
917 km |
495 nm |
475 mph |
764 km/h |
cruise speed |
150 mph |
241 km/h |
|
capacity |
Pilot and one passenger |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.