Most of the world highlights the peculiarities of the first prototype stealth fighter F-313 Qaher Iran. A few days ago, MEHR News Agency published an article that explains the features of this aircraft.
Articles about the main features of the 10 F-313 Qaher published MEHR this answers some doubts and his ability to fly, as well as to prove that Iran's new aircraft not only airworthy, but also as one of the most advanced fighter jets in the world. It has also been stated by President Mahmoud Ahmadinejad.
Here are 10 key features, technical characteristics and some relevant data Qaher F-313 MEHR quoted from the article:
1. Using two inlet (air holes). Inlet channel will produce air conduction system to flow into the engine. Since the inlet and engine direct angle, radar reflectivity will be reduced, and the slanted design to the surface of the inlet channel is useful to absorb radar energy waves, such as the F-35 JSF.
2. Hot exhaust gas will mix with the cold air through the duct inlet, and exhaust gas will cool before exiting the exhaust system. This is to reduce the effects of heat on the surface of the plane.
3. The use of radar absorbent material on the body, to absorb wave energy and reduce radar reflection. This is a great effect for the stealth features of the F-313 Qaher.
4. Given the length and height of the aircraft is less than 16 and 4 yards, two compartments with a capacity to carry two 2000-pound bombs, or more for a small smart missiles, or at least 6 missile air-to-air of the type R-17 or PL-12 .
5. Surface tail (the tail) is relatively large and the vertical will create a good directional stability with a tail and vertical slant to create an aerodynamic advantage for lateral maneuverability.
6. The canopy is very large (wide) provides visibility (sight) 360 degrees. It is important for a flight at low altitude, especially to help the ground attack missions and large canopy will be memantu in fighting "dog-fight."
7. The wings were tilted from Qaher F-313 is perfect for airplane wings, which like the letter M or more like a W upside down, is the best wing shape for use on aircraft.
8. Landing gear 1 cycle is another proof that the F-313 is a light aircraft, with a minimum flying weight of 12 to 14 tonnes and a maximum flying weight of 20 tons.
9. There are 8 display (view) analogue in the cockpit, which shows the multi-function display technology (Multi-Function Display / MFD) that provides plenty of room in the cockpit.
10. F-313 steering bertuas normal, control systems, with the moving surface of the wing, rudder, vertical stabilizer and hydraulic systems flown Fly-by-Wire (FBW), because the use of these aircraft many of the control lever (side steering lever).
Computer with advanced software (CATIA) is used to design the F-313, and aerodynamic analysis methods such as Computational Fluid Dynamics (CFD) is also used, with the help of numerical soft tissue (Gambit) the latest, flow analysis software (FLUENT) and design calculations from other software, which generates a complete scientific work in a variety of science and technology for use in the F-313 Qaher.
Yet again, the ten main features of Qaher F-313 is still a unilateral claim of Iran. Just as the end of the article Qaher before, only time will tell.
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