Airbus A310-300 vs. Cessna A-37 Dragonfly
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Airbus A310-300 |
versus |
Cessna A-37 Dragonfly |
46.66 m |
153 ft 1 in |
length |
8.617 m |
28 ft 3 in |
15.8 m |
51 ft 10 in |
height |
2.71 m |
8 ft 11 in |
43.9 m |
144 ft |
wingspan |
10.94 m |
35 ft 11 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 x General Electric J85-GE-17A turbojets |
52,000 lb |
thrust per engine |
2,850 lbs |
104,000 lb |
total thrust |
2 x 2,850 lbs = 5,700 lbs |
148,768 kg |
328,000 lb |
MTOW |
6,350 kg |
14,000 lb |
8,050 km |
4,348 nm |
range |
460 nmi |
852 km |
482 knots |
279 mph |
cruise speed |
489 mph |
787 km/h |
190-230 passengers |
capacity |
3,000 pounds of bombs, rockets and missiles |
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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.