Lockheed Martin F-35 Lightning II vs. Bell 206
... or view the full comparison list
here.
Lockheed Martin F-35 Lightning II |
versus |
Bell 206 |
15.67 m |
51 ft 4 in |
length |
12.11 m |
39 ft 9 in |
4.33 m |
14 ft 2 in |
height |
2.88 m |
9 ft 5 in |
10.7 m |
35 ft 1 in |
wingspan |
|
|
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 |
engines |
1 × Allison 250-C20B |
40,000 lb |
thrust per engine |
420 shp (313 kW) |
40,000 lb |
total thrust |
420 shp (313 kW) |
31,800 kg |
70,000 lb |
MTOW |
1,451 kg |
3,199 lb |
1,380 mi |
1,200 nm |
range |
374 km |
202 nm |
520 kt |
302 mph |
cruise speed |
222 km/h |
138 mph |
18,000 pounds of total ordinance |
capacity |
1 pilot + 4 passengers |
|
|
rotor diameter |
11.00 m |
36 ft 1 in |
|
|
rate of climb |
425 m/min |
1,395 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.