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.

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: 4 x Lyulka AL-7P, 65.7 kN (14,740 lbf) thrust each

Performance

• Maximum speed: 878 km/h (474 kt; 548 mph
• Range: 4,500 km (2,400 nm; 2,800 sm)
• 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

Comparable aircraft:

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