Tupolev Tu-110

   


The Tupolev Tu-110 (NATO reporting name: Cooker) was a prototype Soviet airliner, a four-engined variant of the Tu-104 powered by Lyulka AL-5 turbojets rated at 53.9 kN (12,125 lbf) thrust each. It was first flown in March 1957. A few were built but not ordered by Aeroflot and later served as Air Force flying testbeds.

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Specifications (Tu-110)

General Characteristics

  • Crew: five
  • Capacity: 100 passengers
  • Length: 40.06 m (131 ft 5 in)
  • Wingspan: 36.98 m (121 ft 4 in)
  • Height: 11.53 m (37 ft 10 in)
  • Wing area: 186 m² (2,001 ft²)
  • Empty: kg ( lb)
  • Loaded: kg ( lb)
  • Maximum takeoff: 82,700 kg (181,940 lb)
  • Powerplant: 4x Lyulka AL-7P, 65.7 kN (14,740 lb) thrust each

Performance

  • Maximum speed: 878 km/h (548 mph)
  • Range: 4,500 km (2,813 miles)
  • Service ceiling: 12,000 m (39,360 ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Thrust-to-weight ratio:

Related content

Related development: Tu-16 - Tu-104 - Tu-107 - Tu-124

Comparable aircraft:

Designation sequence: Tu-105 - Tu-106 - Tu-107 - Tu-110 - Tu-114 - Tu-116 - Tu-119


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