YAK _ 130 تشبه كثيرااا طائرة M346 طائرة
The Yak-130 aircraft is a swept mid-wing monoplane of a classical
configuration with two-seat tandem cockpit and two turbofan engines
with 2500 kg thrust each.
Each cockpit of the aircraft is equipped with three multifunctional
colored 6x8 inches LCD displays without electromechanical instruments,
as well as collimator aviation indicator and helmet-mounted target
designation system in forward cabin.
The aircraft aerodynamic configuration and flight and power plant
controls performance make it possible to operate the aircraft
essentially at all flight conditions, typical of modern and advanced
combat aircraft. The aircraft leading edge extensions and air intakes
layout enable a steady controllable flight at angles of attack up to 40
deg.
High thrust/weight ratio provides high sustained maneuvering load factors, takeoff performance and rate of climb.
The air intakes and landing gear design with high take-off/landing
performance make it possible to operate the aircraft from unpaved
runways small unprepared airfields.
The aircraft is equipped with complex fly-by-wire control system that
functions as automatic flight control system, active flight safety
system and provides in training stability and controllability
characteristics change depending on the aircraft being simulated.
The aircraft combat training system provides simulation of:
air combat with tracing, detection, identification, locking-in, and
tracking of air targets, with launching of air-to-air missiles fitted
with radar and IR homing heads, with imitation of enemy missiles and
jamming launching and with application of airborne defensive aids
system;
interaction with other aircraft in group and with ground and air control units;
air-to-ground attacks with launching of air-to-surface missiles fitted
with radar, TV, IR and laser homing heads, with bombs and rockets
releasing, gun firing, with imitation of enemy surface-to-air missiles
and jamming launching and with application of airborne defensive aids
system.
Simplicity of the structure, high reliability of the airframe, power
plant and aircraft systems, long service life and full self-sufficiency
of the aircraft as well as high maintainability together with a low
cost of the life cycle and high flight performance provide high-quality
training of the pilots in the shortest possible time and meet
efficiently different military challenge.
Basic Data:
Mass:
- takeoff, maximum 9 000 kg
- takeoff, normal 5 700 kg
- fuel, maximum:
- in internal tanks 1 750 kg
- in external tanks 2 х 450 kg
- armament, maximum 3 000 kg
Power plant 2 turbofance
Takeoff thrust, ISA 2 х 2 500 kg
Maximum thrust/weight ratio 0,9
Speed:
- level flight, maximum 1 050 km/h
- takeoff (full fuel load) 200 km/h
- landing 195 km/h
Maximum flight altitude 12 500 m
Flight angles of attack < 40°
Service range with maximum internal fuel 2.000 km
Load factor::
- sustained at 4 572 m altitude (15 000 ft 5,2 g
- maneuvering load factor limits +8 g; -3 g
Airfield runway length 1 000 m
Service life 10 000 hours
موضوع: ابرز صفقات الجزائرية من إيطاليا القادمة 
الجمعة 9 نوفمبر - 0:03
