An-124 Ruslan and Su-27s

The Antonov An-124 Ruslan (NATO reporting name: Condor) is a strategic airlift jet aircraft. It was designed by the Antonov design bureau in the Ukrainian SSR, then part of the Soviet Union. The An-124 is the world’s highest gross weight production cargo aeroplane and second heaviest operating cargo aircraft, behind the one-off Antonov An-225.

General characteristics

  • Crew: 4–6 (pilot, copilot, navigator, senior flight engineer (+flight engineer, radio man) + 2 loadmasters)
  • Capacity: 88 passengers or the hold can take an additional 350 on a palletised seating system
  • Payload: 150,000 kg (330,000 lb)
  • Length: 68.96 m (226 ft 3 in)
  • Wingspan: 73.3 m (240 ft 5 in)
  • Height: 20.78 m (68 ft 2 in)
  • Wing area: 628 m² (6,760 sq ft)
  • Empty weight: 175,000 kg (385,000 lb)
  • Loaded weight: 405,000 kg (893,000 lb)
  • Useful load: 230,000 kg (508,000 lb)
  • Max. takeoff weight: 405,000 kg (893,000 lb)
  • Powerplant: 4 × Ivchenko Progress D-18T turbofans, 229.5 kN (51,600 lbf) each

Performance

  • Maximum speed: 865 km/h (467 kn (537 mph))
  • Cruise speed: 800–850 km/h (430 kn (490 mph))
  • Range: 5,200 km (2,808 nm, 3231 mi)
  • Service ceiling: 12,000 m (39,370 ft)
  • Wing loading: 365 kg/m² (74.7 lb/sq ft)
  • Thrust/weight: 0.23
  • Take-off run distance (maximum take-off weight): 2,520 m (8,270 ft)
  • Landing roll distance at maximum landing weight: 900 m (3,000 ft)

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