Airbus A310-300 vs. Avro Shackleton

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Airbus A310-300 versus Avro Shackleton
46.66 m 153 ft 1 in length 26.6 m 87 ft 4 in
15.8 m 51 ft 10 in height 6.22 m 20 ft 5 in
43.9 m 144 ft wingspan 36.58 m 120 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 x Rolls-Royce Griffon 57
52,000 lb thrust per engine 1,960 horsepower
104,000 lb total thrust 7,840 horsepower
148,768 kg 328,000 lb MTOW 39,009 kg 86,000 lb
8,050 km 4,348 nm range 3,621 km 1,955 nm
482 knots 279 mph cruise speed 262 kts 163 mph
190-230 passengers capacity 10,000lb of bombs, torpedoes or mines
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.