Airbus A310-300 vs. North American F-100 Super Sabre
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Airbus A310-300 |
versus |
North American F-100 Super Sabre |
46.66 m |
153 ft 1 in |
length |
16.46 m |
54 ft 2 in |
15.8 m |
51 ft 10 in |
height |
4.93 m |
16 ft 2 in |
43.9 m |
144 ft |
wingspan |
11.84 m |
38 ft 1 |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
1 Pratt & Whitney J57-P-21A |
52,000 lb |
thrust per engine |
16,000 lb. thrust in afterburner |
104,000 lb |
total thrust |
16,000 lb. (afterburner) |
148,768 kg |
328,000 lb |
MTOW |
17,609 kg |
38,800 lb |
8,050 km |
4,348 nm |
range |
2,673 km |
1,444 nm |
482 knots |
279 mph |
cruise speed |
587 mph |
945 km/h |
190-230 passengers |
capacity |
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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.