Tupolev Tu-110

Tupolev Tu-110

__NOTOC__The Tupolev Tu-110 (NATO reporting name: Cooker) was a prototype Soviet airliner, a four-engined version of the Tu-104 powered by Lyulka AL-5 turbojets rated at 5,500 kgf (53.9 kN; 12,100 lbf) thrust each, two engines on each wing. It was first flown in March 1957.Only 3 where built but none ordered by Aeroflot nor any other airline and they later served as Air Force flying testbeds. This aircraft was intended for export due to the limited export sales of the
Tu-104, Tupolev thought a four-engined plane would be easier to sell due to ETOPS regulation. This aircraft was also fitted with drogue parachutes and use of it could shorten the landing run up to 400 meters.

Specifications (Tu-110)

aircraft specification
|plane or copter?= plane
jet or prop?= jet
crew=5
capacity=100 passengers
length main=40.06 m
length alt=131 ft 5 in
span main=36.98 m
span alt=121 ft 4 in
height main=11.53 m
height alt=37 ft 10 in
area main=186 m²
area alt=2,000 ft²
airfoil=
empty weight main=
empty weight alt=
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main=82,700 kg
max takeoff weight alt=182,300 lb
more general=

engine (jet)=Lyulka AL-7P
type of jet=
number of jets=4
thrust main=6,700 kgf
thrust alt=65.7 kN
thrust original=14,700 lbf
afterburning thrust main=
afterburning thrust alt=

max speed main=878 km/h
max speed alt=546 mph
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main=4,500 km
range alt=2,800 sm
ceiling main=12,000 m
ceiling alt=39,400 ft
climb rate main=
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=

armament=

avionics=

ee also

aircontent
see also=
related=
*Tu-16 -
*Tu-104 -
*Tu-107 -
*Tu-124
similar aircraft=
sequence=
lists=


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