Tupolev Tu-110
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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 (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
Template:Tupolev Russian airliners
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