Airbus A310-300 vs. Lockheed Ventura
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Airbus A310-300 |
versus |
Lockheed Ventura |
46.66 m |
153 ft 1 in |
length |
15.7 m |
51 ft 5 in |
15.8 m |
51 ft 10 in |
height |
3.6 m |
11 ft 10 in |
43.9 m |
144 ft |
wingspan |
20 m |
65 ft 7 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 x Pratt & Whitney R-2800 radial engines |
52,000 lb |
thrust per engine |
2,000 hp |
104,000 lb |
total thrust |
4,000 hp |
148,768 kg |
328,000 lb |
MTOW |
15,000 kg |
33,100 lb |
8,050 km |
4,348 nm |
range |
2,670 km |
1,440 nmi |
482 knots |
279 mph |
cruise speed |
230 mph |
370 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.