NO1 F-22 Raptor Fighter
The F-22, the world's first and only fourth-generation supersonic fighter in production, which has "supersonic cruise, super maneuverability, stealth, maintainability," become the de facto standard for the fourth generation of supersonic fighters. The fact that it has "supersonic cruise, super maneuverability, stealth, maintainability" has become the fourth generation of supersonic fighters the de facto standard.
Radar Reflective Surface = two sheets of A4 paper
The F-22 is a next-generation fighter that the U.S. Air Force has commissioned Lockheed, Boeing and General Dynamics to work together on. For the first time, the program called for five characteristics to be concentrated in a single aircraft: low detectability, high maneuverability and agility (stealth), the ability to cruise at supersonic speeds (as opposed to sprinting at supersonic speeds for short periods of time), and a high payload with a sufficiently long range.
The F-22 has a wingspan of 13.56 meters; a fuselage length of 18.92 meters; a height of 5 meters; and a wing area of 78.80 square meters.
The F-22 adopts a dual-vertical-tail twin-engine, single-seat layout. The vertical tail is tilted outward at 27 degrees, just at the edge of the general stealth design. Its two sides of the air intake in the wing below, and has a stealth design to inhibit infrared radiation, the main wing and flat tail with a consistent swept back angle and trailing edge of the swept back angle, blister-shaped cockpit cover protrudes from the fuselage in front of the upper part of the fuselage.
Special shapes and coatings that absorb radio waves give the fighter an effective radar reflection area of only about 0.1 square meters, comparable to the area of two sheets of A4 paper.
The powerplant is powered by two F119-PW-100 turbofan engines with afterburners. Maximum flight speed is 1,950 kilometers per hour, maximum near-ground flight speed is 1,480 kilometers per hour, actual maximum flight altitude is 18,000 meters, and the combat radius is about 1,500 kilometers. the F-22 can fly continuously for 30 minutes without the engines on boost at Mach 1.58 (Mach 1 is equivalent to 1x the speed of sound).
Modern war, the status and role of over-the-horizon air combat is becoming more and more prominent, so the F-22's over-the-horizon combat capability in the design phase is extremely important. F-22 fighter aircraft using medium-range air-to-air missiles are mainly AIM-120C, which is said to be "launched regardless of the new generation of air-to-air missiles with active radar-seeking, auto-guided capabilities. radar seeking, automatic guidance capabilities. Can be outside the visual range for precision strikes, with the stealth capabilities of the aircraft, so that the F-22 can be the first enemy to find the target, the first enemy launch weapons, master the battlefield initiative.
The F-22 has three internal weapons bays, two of which are arranged along the air intakes and can hold AIM-9 missiles; the other is in the lower fuselage and can hold six AIM-120C medium-range air-to-air missiles. For ground attack missions, the lower fuselage weapons bay can also be equipped with two AIM-120C missiles and two JDAM-1000 guided bombs and sub-tanks at a weight of 454 kilograms. The F-2 is also equipped with an internal machine gun, the M61A2.
Air-to-ground versatility
As a "fourth-generation fighter," the F-22 is also a multi-purpose fighter that can be used for both aerial combat and powerful ground attack capabilities. The F-22 is also a multi-purpose fighter that can be used for both air combat and a powerful ground attack capability. Multi-purpose aircraft have the following advantages: first, it is conducive to shorten the development cycle, secondly, it can save development funds, and thirdly, it is conducive to improve the operational flexibility and overall combat capability
NO2 Su-37 Fighter
Russia's Sukhoi Company developed a single-seat, twin-engine, multi-purpose fighter aircraft on the basis of the Su-35, which made its debut in April 1996, and which uses a tri-wing aerodynamic system. The aircraft adopts a three-wing aerodynamic layout and thrust vectoring control technology, equipped with two AL-37UF thrust vectoring engines, a single maximum additive thrust of 180 kN, thrust-to-weight ratio of 8.7. The aircraft length of 22.2 meters, height of 6.4 meters, wingspan of 14.7 meters, the maximum takeoff weight of 34 tons, the maximum level flight speed of Mach 2.35, the practical limit of lift of 18,800 meters, a maximum range of 3,300 km (6500 km with one air refueling), a maximum of 3,300 km (the maximum range of 1,500 km with one air refueling). The maximum range is 3,300 kilometers (6,500 kilometers with one air refueling), and the combat radius is 1,400 kilometers. The nose of the aircraft is equipped with a N011M phased-array fire control radar, the maximum detection range of 150 kilometers, can simultaneously track 15 targets, and can simultaneously attack six of them; the tail of the aircraft is equipped with a rear-view radar, which can be attacked on the tailing target. Airborne weapons have a 30 mm gun, 17 external hangers, can hang 14 air-to-air missiles, including R-73 close combat air-to-air missiles missiles, R27/77 medium-range air-to-air missiles, but also can carry Kh/29/31/41/59 air-to-ground missiles, a variety of bombs and rockets, with a maximum payload of 8,500 kilograms.
NO3 Su-35 Fighter Jet
The power plant of Su-35 is two L-35 turbofan engines with a controlled thrust vectoring system, which improves the maneuverability takeoff and landing performance of the aircraft. New airborne electronic equipment, plus multifunctional Doppler radar, with air-to-air, air-to-ground dual function and anti-jamming capability. The radar of the Su-35 can detect targets such as fighters at a range of 165 to 245 kilometers, and up to 400 kilometers for bombers, AWACS or large transport aircraft. It can track 15 air targets at the same time and attack six targets simultaneously with missiles. Su-35 aircraft also for the first time used rear-view fire control radar technology, which can guide the Russian specially developed rear-firing type of close-range air-to-air missiles. Su-35 fighters are equipped with rotating launchers under the wings that can rotate 180 degrees horizontally, which can be rotated automatically or at the pilot's command. In other words, the Su-35 missile can be launched to the rear hemisphere, which is often referred to as "over-the-shoulder launch", which is the most unique design of the Su-35.
NO4 F-18 Fighter Jet
The F-18 is a carrier-based fighter jet, and the A-18 is a carrier-based attack jet. As the two are developed on the basis of the same prototype, that is, a machine of two types, the fuselage is exactly the same, only in the armament differences, so collectively referred to as the F / A-1B, nicknamed the same as the "Hornet". 1974 just as the U.S. Air Force put forward the In 1974, when the U.S. Air Force proposed the "Light Fighter" program and began to develop prototypes, the U.S. Navy also proposed the development of multi-role fighter requirements. It was called the VFAX program at the time, but was later renamed the Naval Air Combat Fighter Program. The main fire control equipment includes AN/AVQ-28 flat screen display, AN/AYK-14 central mission computer (2 units), AN/APG-65 pulse Doppler radar, multi-function display, external object management device, AN/AWG-21 antiradiation missile (AGM-78) controller and so on. Models performing air-to-ground attack have some variations of displays in the cockpit and are equipped with forward-looking infrared (FLIR) and laser spot tracker (LST).
The aircraft has a wingspan of 11.43 meters, a length of 17.07 meters, and a height of 4.66 meters; a takeoff weight of 15,740 kilograms (air combat) and 22,328 kilograms (ground attack); a maximum level flight speed of 1,910 kilometers per hour (at high altitude), a useful ceiling of 15,240 meters, and a radius of operations of 740 kilometers (air combat), 1,065 kilometers (ground attack), and a turnaround range of 3,700 kilometers (without aerial refueling). The airborne equipment includes the Hughes AN/AGP-65 multi-function digital air-to-air and air-to-ground tracking radar, which can track 10 targets and display 8 targets to the pilot during air-to-air operation. In addition, the ALR-67 radar alert receiver, four degrees of flight control system and two AYK-14 digital computers, as well as Leighton inertial navigation system, two Kaiser multi-function displays, and Ferendi / Bendix center-type on-screen display and visual display.
NO5 Mirage 2000
The Mirage 2000 is a very distinctive third-generation fighter, it is the only third-generation fighter that has been put into service in the delta-winged aircraft without a front Il. It can be said that this is a unique third-generation aircraft. France in the development of fighter aircraft in a unique practice is not only reflected in the "Mirage" 2000 aircraft, but also reflected in the formation and development of the entire "Mirage" series of aircraft.
Multiple types of aircraft and multi-purpose, is the "Mirage" aircraft "heritage", "Mirage" 2000 aircraft is no exception. Its basic type is the air superiority fighter 2000C, can be attempted all-weather, full-height / all-round, long-range interception mission; soon developed 2000B two-seat trainer type and 2000N ground attack type, and recently developed a significantly improved air combat capability of the 2000-5 type. In addition, some other modifications are also being developed. For an economic strength is not very strong, the number of equipment required is not too many countries, this "multi-purpose" aircraft is more suitable, but also conducive to exports and compete for foreign users.
NO6 Typhoon Fighter
The birth of the Typhoon took a few twists and turns. in the mid-1980s, several major European countries, Britain, France, Germany, Italy, Spain and other brewing *** with the development of a "future European warplane", used to replace the last generation of the countries of the "Rapids" and other fighters, is expected to be in service in the mid-1990s. Due to a disagreement over the design of the aircraft, France withdrew from the project and developed the Rafale alone." The 'Future Eurofighter' program was also delayed again and again, and changed its name several times, first renamed "Eurofighter 2000" (EF2O00), then called "EurofIghter" (EurofIghter), and finally named "Typhoon" (Typhoon).
"Typhoon" fighter 14?96 meters long, wingspan 10?95 meters, 5?28 meters high, the power plant is two turbofan engines, the maximum lifting capacity of about 21 tons, the maximum speed of 2,125 km / h. The Typhoon is a kind of air combat and take the lead. Belong to a kind of air combat and seize the right to control the air mainly, both ground and sea attack ability of medium-sized fighters.
NO7 F-15 Fighter
The F-15 is a heavy air-to-air fighter developed by McDonnell Douglas. The F-15 is a heavy air-to-air fighter developed by McDonnell Douglas. It is mainly used to seize air control, and can also be used for ground attack. The U.S. Air Force selected the McDonnell Douglas design in 1969. Road company's design program and let it develop 20 prototypes, the first test flight in July 1972, in November 1974 began to deliver troops to use. In addition to the U.S., Israel, Japan, and Saudi Arabia are also equipped with the F-15.
The F-15 has a single-seat, twin-engine, twin-piton-tailed upper monoplane layout. The wing planform is triangular, and the wing has no leading edge maneuvering flaps. The fuselage structure of a large number of titanium alloy. F-15 thrust-to-weight ratio, wing load small, maneuverability, with a selection of electronic preparedness, especially for close combat and over-the-horizon missile attack. In the 1991 Gulf War, 120 F-15s took part in the battle, mainly responsible for air control and escort tasks, and shot down a number of Iraqi fighters
NO8 J-10 fighter
J-10, according to the western division of the method of fighter, belongs to the typical third-generation fighters. J-10 will be China's first self-designed, third-generation fighter equipped for use by the troops, the first self-designed, truly both air superiority/ground dual combat capability of combat aircraft. Unfortunately, the J-10 has not been officially launched since 1984 and has yet to enter service.
The J-10 can be considered one of the most mysterious fighters in the history of the Chinese air force. Since the outside world first discovered its existence, all kinds of rumors about it have been uninterrupted. Some say that it is technologically advanced and unrivaled, while others say that it has had many difficulties in its development. So what kind of airplane is it?
Length: 14.57 meters
Height: 4.78 meters
Wingspan: 8.78 meters
Maximum takeoff weight: 19,277 kilograms
Engine: 1 x AL-31FN turbofan or Turbofan-10A turbofan
Maximum thrust: 112.6 kilonewtons (AL-31FN)
Maximum thrust: 1 x AL-31FN or Turbofan-10A turbofan
Maximum thrust: 112.6 kilonewtons (AL 31FN)
Maximum flight speed: Mach 2+
Transit range: greater than 3,000 km
Maximum overload: 7g (sustained)/10G (instantaneous)
NO9 INDIAN LCA FIGHTER
The LCA is the world's smallest fighter, weighing in at 5.5 tons, with 40% of the fuselage composed of composite materials The LCA is the smallest fighter aircraft in the world, weighing 5.5 tons. It has twin delta tailless wings and a vertical horizontal tail. It is powered by a Kaveri engine. The design of the delta wings makes the LCA very agile and provides it with excellent maneuverability.The LCA is a fairly modern fighter aircraft in design, it looks like the French Rafale and the Eurocopter.
The LCA's Doppler pulse radar has a range of more than 100KM and can track up to 10 targets simultaneously. It has a four-degree digital flight control system and advanced integrated electronics, and it has a great electronic warfare system. the LCA has a HUD and is also equipped with a helmet mounted sight. the LCA's radar has advanced map mapping capabilities. the LCA has an internal laser locator and an IRST. the LCA will have an open architecture system
NO10 MiG-25 <
The MiG-25 was frequently photographed on the local battlefields of the 1970s and 1980s, especially its reconnaissance version. on the eve of the outbreak of the Fourth Middle East War in the fall of 1971, four Soviet MiG-25R reconnaissance variants were stationed in Egypt and traveled to reconnaissance over Israel from time to time. The Israeli Air Force sent the best Western fighter at the time, the American-developed F-4 Ghosts, to intercept them. The MiG-25P opened up the booster combustion chamber, a moment to throw off the tailing F-4. F-4 hastily launched AIM-9 "Rattlesnake" close air-to-air missiles, trying to missiles tailing the MiG-25, I did not think that even the missiles did not catch up.
In December 1992, a MiG-25 aircraft of the Iraqi Air Force was shot down by U.S. F-16s using AIM-120 "advanced medium-range air-to-air missiles" in the no-fly zone in northern Iraq. The aircraft was shot down by a U.S. F-16 fighter using an AIM-120 Advanced Medium Range Air Missile. But then the Iraqi army in the long-term confrontation summed up the experience and created a new tactic that works, there was a MiG-25 fighter aircraft in the U.S. aircraft were found and launched AIM-120 medium-range air-to-air missiles (before the missile in the actual combat never miss) attack actually able to high-speed turn quickly out of the case, so that the U.S. people were stunned
Weapons: no internal gun, four under the wing mounts with four AA-6 medium-range air-to-air missiles, two infrared-guided on the inside and two semi-active radar-guided on the outside.
Wingspan 13.95 meters
Length 22.3 meters
Height 5.7 meters
Wing area 56.2 square meters
Empty weight 15,000 kilograms, normal takeoff weight 36,000 kilograms, maximum takeoff weight 37,500 kilograms, fuel capacity (internal) 14,000 kilograms
Maximum speed. M3.0/3180km/h (altitude 18,300m), max combat speed M2.8/2970km (altitude 17,000m), utility ceiling 24,000m
Maximum combat radius 1,300km, range 3,000km