Airbus A310-300 vs. North American Rockwell OV-10 Bronco
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Airbus A310-300 |
versus |
North American Rockwell OV-10 Bronco |
46.66 m |
153 ft 1 in |
length |
12.7 m |
41 ft 7 in |
15.8 m |
51 ft 10 in |
height |
4.62 m |
15 ft 2 in |
43.9 m |
144 ft |
wingspan |
12.19 m |
40 ft |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 x Garrett T76-G-420/421 turboprop engines |
52,000 lb |
thrust per engine |
Approximately 715 hp each |
104,000 lb |
total thrust |
Approximately 1,430 hp total |
148,768 kg |
328,000 lb |
MTOW |
14,444 lb |
6,553 kg |
8,050 km |
4,348 nm |
range |
1,931 km |
1,043 nm |
482 knots |
279 mph |
cruise speed |
244 mph |
393 km/h |
190-230 passengers |
capacity |
Pilot and observer |
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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.