Thursday, May 31, 2012

Aircraft Tu-134UB-L


In the late 70's OKB been developing a training aircraft for pilots training with long-range aviation aerobatic qualities inherent in combat vehicles. Originally supposed to do it on the basis of the draft passenger Tu-136, but settled on a modification of the Tu-134B, satisfies the requirements for pilot training Tu-22M.

Tu-134UB-A with D-30 engines, 2nd series was designed for training pilots piloting instrument in simple and adverse weather conditions, air navigation, landing in director or automatic modes. The plane had to fly in a minimum of 2 nd category ICAO. Unlike its predecessor, the Tu-134UB-A installed a new forward fuselage, similar to the Tu-22M-3 radome radar ╚ ROSE-1 ╩.

The initial project involves the installation of machines in the nose of the bar system in-flight refueling, but due to the removal of similar equipment from the Tu-22M, it was abandoned. According to the composition of equipment it is mostly consistent with the Tu-134B, except for radio communication and navigation systems, typical of combat vehicles. For students and 12 seats were designed to scan, set in three rows. In flight, the cadets were trained at a time as the second pilot.



The first machine was built on the HAPO in January of 1981 until spring released several production aircraft, has successfully passed together with the customer flight tests. Before the 1983rd association deposited 90 Tu-134UB-A. For naval aviation produced a copy of the modified Tu-134UB-K for training navigators, navigators, and navigators, operators of the Tu-22M.

Thursday, May 24, 2012

Aircraft Tu-154M




The Tu-154 is an extension of the well-known jet Tu-154V medium-range missiles.Due to improvements made ​​by the aerodynamic and installing more efficient engines D-30KU significantly improved characteristics of the aircraft in terms ofspecific fuel consumption. Created in the Yakovlev Design Bureau. Tupolev.



Aircraft performance
Equipage
3 persons
Cruising speed 
950 km/h
Flight range
5200 km.
Maximum payload
18 tones
Length required for take-off and landing 
2500 m.
The maximum takeoff weight
100 tones
Maximum landing weight
80 tones
Maximum weight without fuel
74 tones
Maximum weight of fuel
39,75 tones
Maximum passengers
180-160 persons
Fuel consumption
5,4 tones an hour

Aircraft Tu-154B



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.