Lockheed Martin F-22 Raptor vs. de Havilland Canada DHC-6 Twin Otter
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Lockheed Martin F-22 Raptor |
versus |
de Havilland Canada DHC-6 Twin Otter |
18.9 m |
62 ft 1 in |
length |
15.32 m |
50 ft 3 in |
5.1 m |
16 ft 9 in |
height |
5.94 m |
19 ft 6 in |
13.6 m |
44 ft 7 in |
wingspan |
19.81 m |
65 ft |
Two Pratt & Whitney F119-PW-100 turbofan engines |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
35,000-pound class |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
70,000-pound class |
total thrust |
1100 to 1500 shaft horsepower |
38,000 kg |
83,500 lb |
MTOW |
5,670 kg |
12,500 lb |
1,850 mi |
1,611 nm |
range |
1,389 km |
750 nm |
Mach 1.6 |
1976 km/h |
cruise speed |
280 km/h |
174 mph |
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capacity |
19 passengers |
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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.