The Tu-154 passenger jet is the middle range and is
designed for use on routesextending from 500 to 4000km. Three
power-efficient engine with low specific fuel consumption of a good power-to
provide an aircraft and a large range.The complex flight and navigation
equipment provides automatic flight and automatic approach for the two
categories of ICAO. Endurance aircraft maintenance is achieved by using on
board auxiliary power unit, which provides a self-startengines, air
conditioning systems work in salons while parked and taxiing aircraft, testing
of all systems on the ground without starting the main engines.Created in the
Yakovlev Design Bureau. Tupolev.
Aircraft performance
Equipage
|
3 persons
|
Cruising
speed
|
900 - 950
km/h
|
Height of
up
|
12000 m.
|
Flight
range
|
3250 km.
|
Required
runway lenght
|
2200 m.
|
The
maximum takeoff weight
|
96000 kg.
|
Maximum
landing weight
|
78000 kg.
|
Maximum
payload
|
18000 kg.
|
Maximum
passengers
|
169
|
Maximum weight of fuel
|
39,7 tones
|
Power plant
The power plant consists of three turbojet bypass engines with thrust reversers(NK8-2U). Take-off thrust of one engine sostovlyaet 10 500 kg, fuel consumption is 6.2 tons hour. Start engines produced by the auxiliary power unit, which is locatedin the rear fuselage. The side engines reverse thrust with the device that reduces the length of the landing run.
The power plant consists of three turbojet bypass engines with thrust reversers(NK8-2U). Take-off thrust of one engine sostovlyaet 10 500 kg, fuel consumption is 6.2 tons hour. Start engines produced by the auxiliary power unit, which is locatedin the rear fuselage. The side engines reverse thrust with the device that reduces the length of the landing run.
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