Lockheed Martin F-35 Lightning II vs. North American BT-9
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Lockheed Martin F-35 Lightning II |
versus |
North American BT-9 |
15.67 m |
51 ft 4 in |
length |
8.79 m |
28 ft 10 in |
4.33 m |
14 ft 2 in |
height |
2.82 m |
9 ft 3 in |
10.7 m |
35 ft 1 in |
wingspan |
10.97 m |
36 ft |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
1 x Wright R-975-3 radial engine |
40,000 lb |
thrust per engine |
Approximately 440 hp |
40,000 lb |
total thrust |
Approximately 440 hp |
31,800 kg |
70,000 lb |
MTOW |
4,300 lb |
1,950 kg |
1,380 mi |
1,200 nm |
range |
917 km |
495 nm |
520 kt |
302 mph |
cruise speed |
150 mph |
241 km/h |
18,000 pounds of total ordinance |
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.