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Su-27 AIRCRAFT DERIVATIVES
The design and aerodynamic configuration of the Su-27 aircraft made it possible to develop a number of combat aircraft derivatives, such as:
- a multirole fighter;- a two-seat (side-by-side seating) strike aircraft;- a two-seat (tandem seating) fighter trainer;- carrier-based fighters (one-seat combat aircraft and two-seat combat trainer).
The multirole fighter development program was targeted to optimize engineering solutions associated with equipping the aircraft with new avionics (including a phasedarray radar, satellite navigation equipment, a multifunctional display- based cockpit indic...
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An-72 LIGHT MILITARY TRANSPORT AIRCRAFT
The An-72 light military transport aircraft is intended to airdrop airborne troops, airlift troop forces with organic combat materiel and armament, rapidly deliver armament and ammunition for troop forces, and evacuate the wounded and sick.
The An-72 boasts short takeoff and landing due to wing high-lift devices and increased thrust-to-weight ratio. Wing-mounted high-set engines avoid an ingestion of foreign objects from the ground and ensure an increase in lift coefficient during takeoff and landing due to an ejection of engine exhaust efflux over the upper wing surface and trailinged...
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Tu-142M ANTISUBMARINE WARFARE AIRCRAFT
The Tu-142M is intended to search for, track and destroy hostile submarines in far-off areas of the ocean (sea) at any time of the day and year, in VFR and IFR weather conditions.
It is developed from the Tu-142 aircraft. The airborne equipment of the aircraft ensures automatic and semiautomatic flights, sonar and magnetometric search, long-time tracking and destruction of enemy submarines. It includes radar, sonar, computer and tactical situation display systems, airborne search magnetometer and hydrological reconnaissance equipment. Sonabuoys are part of its dedicated equipment.
ASW weap...
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R13-300 AFTERBURNING TURBOJET ENGINE
The R13-300 afterburning turbojet engine is intended to power the MiG-21, Su-15M and Su-15TM aircraft. The engine is designed around a twoshaft configuration. For the first time, it was equipped with a slotted spacer over the first stage to enhance low-pressure compressor stability, as well as an afterburner with a radialannular stabilizer and a heat shield perforated with small-diameter holes.
The R13F-300 engine version is intended to power the MiG-21STM/SMF aircraft. The engine is provided with an additional power augmentation mode - emergency rating that enables it to increase the augme...
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WEAPONS CONTROL SYSTEM MODERNIZATION
Type units for upgrading of weapons control systems are based on modern high-tech components and are configured from unified modules according to the 3U design (Euromechanics).The type array of units makes it possible to:- configure an autonomous subsystem to control new air attack weapons (for example, the RVV-AE missile) for the existing fleet of aircraft;- rapidly build up the array of air attack weapons for the existing aircraft by including additional units into the weapons control system;- increase combat effectiveness and engineering level of avionics (by replacing analog interface unit...
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E-95 AERIAL TARGET DRONE
The E-95 is intended to simulate guided aerial bombs, cruise missiles and other unmanned flying vehicles during combat training of personnel of the Air Force, Air Defense, Ground Forces and Navy, and testing of various armament systems.
The E-95 has a straight-wing V-shaped tail airplane configuration and is powered with a pulsating jet engine.
The drone allows to simulate a wide range of training targets for various surface-to-air and air-to-air guided weapon systems due to changing its effective reflective area by specially provided means.
The E-95 is provided with the following...
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RD-33 AFTERBURNING TURBOFAN ENGINE
The RD-33 engine is intended to power the MiG-29 fighter and its modifications.
The RD-33 is a double-flow two-shaft turbofan engine with flow mixing in a common afterburner. The engine is equipped with a fully-variable supersonic exhaust nozzle.
Structurally, the engine comprises a four-stage low-pressure axial flow compressor, a nine-stage high-pressure axial flow compressor, a short annular combustion chamber, singlestage low- and high-pressure turbines, an afterburner bypass air duct, and an adjustable exhaust nozzle. The engine is provided with an electronic/ hydromechanical control and monitoring system.
The RD-33 is designed around a modular configuration. Owing to its high gas-d...
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