Airbus A310-300 vs. de Havilland Venom
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Airbus A310-300 |
versus |
de Havilland Venom |
46.66 m |
153 ft 1 in |
length |
6.71 m |
22 ft 0 in |
15.8 m |
51 ft 10 in |
height |
1.88 m |
6 ft 2 in |
43.9 m |
144 ft |
wingspan |
12.7 m |
41 ft 8 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
1 (de Havilland Ghost 105) |
52,000 lb |
thrust per engine |
23.6 kN |
104,000 lb |
total thrust |
23.6 kN |
148,768 kg |
328,000 lb |
MTOW |
6,945 kg |
15,300 lb |
8,050 km |
4,348 nm |
range |
1,730 km |
935 nm |
482 knots |
279 mph |
cruise speed |
1030 km/h |
640 mph |
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.