Control:

AG1 is the switch that controls the hatch cover, AG2 is the start of the afterburner system, AG3 is the extension of the fuel filler, AG4 is the opening of the night light, AG5 is the abandonment of the attachment, AG6 is the folding wing (remember not to fold it during flight), and AG7 is the retraction and release of the landing hook.

Gallery

background:Project 1143.6 Ativation Crusier Vargay

FROM THR SU-33

performance parameter

The Su-33 has a total length of 21.19m, a wingspan of 14.7m, a folded height of 5.93m and an empty weight of 18400kg. Powered by two AL-31F afterburner turbofan engines, the maximum flight speed reaches Mach 2.17, the maximum takeoff weight is 33000 kg, the practical ceiling is 17000 meters, and the range is 3000 kilometers.

weapons system

The external load of "Su-33" has reached 6500kg. During the implementation of the fleet defense and control mission, it mainly uses missile weapon systems for air combat. In terms of air-to-air missiles, it carries R-27 medium range air-to-air missiles, R-73 short-range combat air-to-air missiles, and uses new KH-41 large supersonic ship launched missiles. This missile was developed by the former Soviet Union in the early 1980s, and its shape is like a magnified version of KH-31, Four solid rocket motors are installed in the middle and rear section of the missile body, which is its biggest feature. The rocket engine is equipped with two groups of foldable springs and KH-41 power system. The integral rocket ramjet engine is used. The maximum speed is close to Mach 3, and the maximum range can reach 250 kilometers. It has strong penetration and anti-jamming capabilities. With a large charge of warheads, a single hit can cause serious damage to large warships. Due to its fast speed and powerful warheads, it is an air launched anti-ship missile feared by many maritime powers.The Su-33 can also be used as rockets and aerial bombs of various calibers. The Su-33 is also equipped with a 30mm GSH-301 machine gun with 150 rounds of ammunition.

Structural characteristicsIn terms of overall structure

the fuselage structure of the Su-33 is basically the same as that of the Su-27, which is composed of the front fuselage center wing and the rear fuselage. In order to enable the Su-33 to withstand the 5G longitudinal overload force generated by difficult blocking during landing, the main load-bearing structure of the Su-33 fuselage has been strengthened. The front landing gear strut is directly connected to the airframe structure, and the structural strength of the front landing gear has also been upgraded. The front wheels are replaced with double wheels. Through the strengthened structure and hydraulic damping system, in order to make the main landing gear bearable, the main landing gear is directly connected to the tail beam at the side of the airframe when arresting the sinking rate of 6~7 meters per second during landing on the ship, and the tail hook assembly is installed on the strengthened central beam, The safety of aircraft taking off and landing on the ship is improved by shortening the length of the tail cone in design, and making great changes to the wing, including the increase of the area of the main wing, and the change of the integral flap aileron with the trailing edge half span to two double slit lift flaps inside the wing. An aileron is arranged near the wing tip.

Avionics systemIn terms of space configuration

Su-33 adopts the improved N001 radar, which improves the radar's detection capability for surface targets. The photoelectric detection device, an infrared receiving system composed of photodiodes, can detect the rear targets within 60 kilometers. The helmet mounted sight on Su-33 uses infrared light-emitting diodes and photosensitive elements in the cockpit for positioning. The sight is used to aim and lock signals. The infrared fighting missile on the aircraft, whose seeker can follow the helmet sight, uses helmet sight to expand the off axis launching range of the Su-33 missile in close range fighting.The aircraft is also equipped with an automatic landing guidance device matched with the aircraft carrier, through which the Su-33 can have all-weather combat capability.The electronic countermeasure equipment of the aircraft is mainly composed of SPO-15LM, omnidirectional radar warning receiver, controlled active jammer and decoy projectile launcher.

THANKS

thanks toOakland for the screenshots.
thanks to Rafalemmm for the screenshots.