Lockheed Martin F-35 Lightning II vs. North American T-6 Texan
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Lockheed Martin F-35 Lightning II |
versus |
North American T-6 Texan |
15.67 m |
51 ft 4 in |
length |
9.0 m |
29 ft 6 in |
4.33 m |
14 ft 2 in |
height |
3.56 m |
11 ft 8 in |
10.7 m |
35 ft 1 in |
wingspan |
12.8 m |
42 ft |
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
1 x Pratt & Whitney R-1340-AN-1 radial engine |
40,000 lb |
thrust per engine |
Approximately 600 hp |
40,000 lb |
total thrust |
Approximately 600 hp |
31,800 kg |
70,000 lb |
MTOW |
5,617 lb |
2,548 kg |
1,380 mi |
1,200 nm |
range |
1,175 km |
634 nm |
520 kt |
302 mph |
cruise speed |
145 mph |
233 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.