Lockheed Martin F-22 Raptor vs. Bell 206
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Lockheed Martin F-22 Raptor |
versus |
Bell 206 |
18.9 m |
62 ft 1 in |
length |
12.11 m |
39 ft 9 in |
5.1 m |
16 ft 9 in |
height |
2.88 m |
9 ft 5 in |
13.6 m |
44 ft 7 in |
wingspan |
|
|
Two Pratt & Whitney F119-PW-100 turbofan engines |
engines |
1 × Allison 250-C20B |
35,000-pound class |
thrust per engine |
420 shp (313 kW) |
70,000-pound class |
total thrust |
420 shp (313 kW) |
38,000 kg |
83,500 lb |
MTOW |
1,451 kg |
3,199 lb |
1,850 mi |
1,611 nm |
range |
374 km |
202 nm |
Mach 1.6 |
1976 km/h |
cruise speed |
222 km/h |
138 mph |
|
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.