Lockheed Martin F-35 Lightning II vs. Bell 206

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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.