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Top 10 best fighter jet in the world today

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Here is a list in which among my knowledge. We make a list of the most or less detailed top about the 10 best fighter jet in the world today. We have to take into account several factors, not only in the technical specifications of each aircraft but also in the combat experience and the skill of the pilot who also serves a lot in a fighter. Also, all this at the end is the training of the fighter until it is shown in an air combat we do not know exactly who or who is better and there are many factors influencing when it comes to winning or out.

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Best fighter jet in the world today

 Lockheed Martin F-22 Raptor of the USA

Characteristics

It is a fifth-generation twin-engine fighter aircraft conceived in the United States during the 1990s that uses furtive technology. Lockheed Martin is the main contractor of the construction and the F-22 being a member of the Boeing program. It is one of the few aircraft that can maintain the supersonic flight without making use of the additional thrust given by the afterburners (and their high associated fuel consumption)best fighter jet in the world today. This capacity is called supercruise, the F-22 is highly maneuverable, both at supersonic and subsonic speeds.

Furtive technology

The furtive ability of the F-22 is due to a combination of factors, including the general shape of the aircraft, the use of radar absorbing materials, and the care of details such as the hinges or the pilot’s helmet that could provide a radar return best fighter jet in the world today. The effectiveness of this emphasis on furtive characteristics during the design process of the F-22 is difficult to calculate. Although its equivalent radar section is almost non-existent, in early 2009 Lockheed Martin published information from the F-22, showing that it has an equivalent radar section from certain critical angles of -40 dBm² (the equivalent radar reflection of a “steel marble”).

Technical specifications (F-22)

– Crew: 1 pilot
– Weight loaded: 29,300 kg
– Maximum takeoff weight: 38,000 kg
– Fuel capacity: 8,200 internal kg, 11,900 kg with 2 external tanks.
– Maximum operating speed: 2,410 km / h (Mach 2,25)
Supercruise: 1,963 km / h (Mach 1,82)
– Scope: 2,960 km with 2 external tanks.
Reach on Ferry: 3,219 Km
Action radius: 759 km
– Service ceiling: 19,812 m
– Limits of forces G: -3.0 / +9.0

Eurofighter Typhoon of the European consortium

Characteristics

The Eurofighter Typhoon is in service in England, Germany, Italy, Spain, Austria and Saudi Arabia. It is a versatile, twin-engine and highly maneuverable fighter, designed and built by the consortium of European companies. He made his first flight on March 27, 1994, entering service on April 8, 2003, in Germany. This fighter is characterized by its great agility both in supersonic flight and at low speeds thanks to its delta/canard design. This design is unstable in flight by nature and has been designed to guarantee its high maneuverability. For this reason, it has a “fly-by-wire” fully digital quadruple redundancy flight control system in charge of providing artificial stability.

Technical specifications 

– Crew: 1 pilot
– Weight loaded: 15,550 kg
– Maximum take-off weight: 23,500 kg
– Maximum operating speed: 2,410 km / h (Mach 2,5)
Supercruise: Mach 1.3 in supersonic flight without afterburner.
– Scope: 1,390 km
Reach by ferry: 3,706 km using 3 external fuel tanks.
– Service ceiling: 19,812 m
– Load alar: 311 Kg
– Ascent regime: 315 m / s.
– Limits of forces G: + 9 / -3

Sukhoi Su-35 Russian, best fighter jet in the world today

 

Characteristics

The Su-Sui Su-35 initially called Su-27M, is a versatile, heavy and long-range fighter, belonging to the Russian 4 ++ generation. The Su-35 is in service in a small number with the Russian Air Force, 12 in the year 2008. Although several designs were tested with front wings “Canards”, the design team of the factory Sujoi OKB, finally made the decision of Do not install these front wings in the new Su-35BM due to the higher air resistance of these ailerons.

Due to similar characteristics and the components it contains, the Su-35 is considered a close cousin of the Su-30 air superiority fighter. Russia has installed the nozzles of escapes orientable, that will allow to the new fighter Su-35 to have vector thrust of a form similar to the American hunting F-22 Raptor, which attributes a high exceptional maneuverability to him with variable thrust.

Technical specifications (Su-35)

– Crew: 1 pilot
– Weight loaded: 25,300 kg
– Maximum takeoff weight: 34,500 kg
– Maximum speed: 2,390 km / h; (Mach 2.25)
Speed at low altitude: 1,400 km / h (Mach 1,14)
– Range: 3,600 km
Reach by ferry: 4,500 km with external fuel tanks
– Service ceiling: 18,000 m
– Alar load: 408 kg
– Ascent regime: 280 m / s
– Limits of forces G: + 9 / -3

Dassault Rafale Frances

Characteristics

Medium-weight, twin-engine, multi-purpose fighter plane, with a delta-wing design and canard’s front wings, in a Delta-canard design combination of the fourth generation of jet fighters, comparable to a generation 4+ fighter designed and built in France, it is in service in the French Air Force and French Naval Aviation, with both bodies expected to become the main aircraft during the first third of the 21st century. The new M88-2 engine specially designed to equip the Rafale must remain in flight at low altitude, with a low specific fuel consumption (and therefore has a high compression ratio of 24.5 and high-performance components), as well also, I needed to fly at high altitude with a specific high impulse (and therefore, a low coefficient of 0.3).

Technical specifications

– Crew: 1 pilot
– Weight loaded: 14,016 kg
– Maximum take-off weight: 24,500 kg
– Maximum operating speed: 2,390 km / h (Mach 2).
Speed at low altitude: 1,390 km / h
– Range: 3,700 km
Action radius: 1,852 km
– Ascent regime: 304.8
– Service ceiling: 16,800 m
– Alar load: 306.6 kg

Boeing F / A-18 Super Hornet from the USA

Characteristics

The new Super Hornet, twin-engine and double-drift heavy fighter is 20 percent larger, 3,000 kg heavier empty, and 6,800 kg heavier, fully loaded with weapons and fuel, than the previous design of the medium-weight fighter Hornet. original. In addition, it can carry 30 percent more internal fuel, thus increasing its range by 41 percent and its strength, 50 percent over the Hornet.

The Air Forces will update Up-grade 4.75th generation due to the delays in the delivery of the F-35C fighter version on board, with more furtive capabilities and a greater range, its update would only be included until the 2024 date by which it is foreseen that Download the Super Hornet for a fifth generation fighter. It is claimed that the Super Hornet employs more equivalent radar section reduction measures than any other contemporary fighter, with the exception of fifth generation F-22. It is not a true poacher like the F-22 but it has a lower frontal RCS than the previous generation of fighters.

Technical specifications (F-18 Super_Hornet)

– Crew: 1 pilot
– Weight loaded: 21,320 kg
– Maximum takeoff weight: 29,900 kg.
– Maximum speed: 1,900 km / h (Mach 1,8)
Speed at low altitude: 1100 km / h (Mach 1).
– Range: 2,361 km
Reach by ferry: 3,334 km
Action radius: 722 km
– Service ceiling: 15,240 m
– Alar load: 453.1 kg

Mikoyan MiG-35 Russian

Characteristics

The Mikoyan MiG-35 is a 4+ generation multipurpose fighter. The new bomber fighter has so many “technological advances” incorporated into its new design, Up-grade upgrades and greater weight, it is more powerful, agile and faster than the previous MiG-29 fighter, with new and powerful vector thrust engines can tilt in any direction, up, down, right or left, independently; It is also possible to tilt the two nozzles in a cross, which allows to have more forward thrust and more lifting speed, something very necessary in a modern aerial combat, to achieve a greater advantage over the opponent and acquire a flight regime.

This has an improved range of over 2,100 km. with external fuel tanks and refueling capability in flight. It has the new turbine engines with “vectorial push”, which are heavier than conventional engines, but by the new aerodynamic design of the aircraft, they allow you to perform all kinds of aerial maneuvers, stop in the air and turn on your own axis, without the need for the canard’s front wings of the new “High maneuverability” Su-30MK fighter.

Technical specifications (Mig-35)

– Crew: 1 pilot
– Weight loaded: 17,500 kg
– Maximum takeoff weight: 24,500 kg.
– Maximum speed: Mach 2.2 at 3,000 m altitude.
The speed at low altitude: Mach 1.4.
– Alcan’s with external fuel tanks: 3,000 km
Reach by ferry: 3,100 km
Action radius: 1,000 km
– Ascent regime: 330 m / s
– Service ceiling: 17,500 m

Sukhoi Mig-29 Russian

Characteristics

The MiG-29 is a fourth generation fighter designed by Mikoyan. It is designed to counter the American fighters of that time, the F-16 Fighting Falcon, and the F / A-18 Hornet. It is a pure fighter, designed for air combat missions against other fighters, at high altitude and speed, of “high maneuverability”, of medium weight, with leading edges that extend from the main wings to the sides of the cabin and with powerful twin engines, installed under the central fuselage. This new design allows the ship to have a “high maneuverability” because the leading edge helps turn the ship. The cockpit maintains a high position, over the main engines and wings, gives the pilot greater visibility in closed dogfight bouts.

Contrary to the unstable design of the western fighter F-16 controlled by Fly-by-wire cables, the MiG-29, bet on a more stable design, but optimized to be more maneuverable, with two large vertical stabilizers, long and extended, over the Twin engines up to the main wings, which offer greater stability at high speed and altitude, and allow tight turns, in extreme combat maneuvers, in combination with its long and extended leading edge, from the main wings to the cockpit. Although there is an analog computer on board the ship, which limits the maneuvers of high Gs and alphas of the fighter, it can be deactivated, allowing the aircraft to be required beyond the established limits, for combat maneuvers in its original design.

Technical specifications (Mig-29)

– Crew: 1 (pilot)
– Empty weight: 11,000 kg
Loaded weight: 29,940 kg
Maximum takeoff weight: 21,000 kg
– Maximum operational speed:
In height: 2,400 km / h (Mach 2,25)
At sea level: 1,500 km / h (Mach 1,25)
– Scope: 1,430 km with maximum internal fuel load
Reach by ferry: 2,100 km with 1 external fuel tank
– Service ceiling: 18,013 m
– Load alar: 442 kg / m²
– Ascent regime: 330 m / s
– Alar load: 483 kg / m²

F-16 Fighting Falcon from the USA

Characteristics

The Fighting Falcon is an aircraft specialized in close air combat that introduced numerous innovations, including a bubble-free cabin without a frame for better visibility, the lateral control lever for better control under high G-forces, and the seat reclined to reduce the effect of G-forces in the pilot. It is expected that the F-16 will remain in service with the United States Air Force until the year 2025. The aircraft that will replace it is the Lockheed Martin F-35 Lightning II, whose entry into service is scheduled for 2016 and that it will gradually replace it.

The propulsion system initially selected for this single-engine aircraft was the Pratt & Whitney turbofan F100-PW-200 with afterburner, a slightly modified version of the F100-PW-100 used by the F-15 Eagle. With a maximum thrust force of 106 kN (23,830 lbs) with afterburning, that model continued as the standard engine of the F-16 until Block 25. The Block 60 aircraft of the United Arab Emirates is powered by the General Electric F110-GE turbofan -132, which with a maximum thrust of 144.6 kN (32,500 lbs), is the most powerful reactor equipped in an F-16.

Technical specifications (F-16)

– Crew: 1 pilot
– Loaded weight: 12,000 kg
– Maximum take-off weight: 19,200 kg
– Maximum operating speed: 2,414 km / h (Mach 2+).
Speed at sea level: 1,470 km / h (915 MPH) (Mach 1,2).
– Reach by ferry: 4.220 km
Range of action: 550 km
– Service ceiling: 18,288 m
– Ascent regime: 254 m / s
– Alar load: 430 kg / m²

Saab 39 Gripe from Sweden


Characteristics

The Saab 39 Gripen is a fighter of the Swedish air force, is an attack aircraft and an aerial reconnaissance aircraft, with a level of performance similar to that of the American F-16. Considered the first “fourth generation” fighter, it is in service in the Czech, Hungarian, South African and Thai Air Forces. Thanks to its new aerodynamic delta wing design, which allows a great capacity of air penetration, with a low radar mark and low thermal mark, at medium altitude, it is totally supersonic and maneuverable, which belong to a previous generation, such as the Dassault Mirage III.

Technical specifications (Saab 39 Gripen)

– Crew: 1 pilot
– Weight loaded: 8,720 kg
– Maximum takeoff weight: 14,000 kg
– Maximum operating speed: 2525 km / h (Mach 2.31)
Speed at sea level: 1400 km / h (mach 1.28)
– Reach in combat: 1260 km
Reach by ferry: 3.940 km
– Service ceiling: 18,500 m
– Ascent regime: 150 m / s
– Alar load: 341 kg / m²
– Limits of forces G: -3.0 / +9.0

McDonnell Douglas F-15 Eagle of the USA

Characteristics

The McDonnell Douglas F-15 Eagle is a twin-engine all-weather tactical fighter designed by the US company McDonnell Douglas since 1997 integrated into Boeing. the F-15E Strike Eagle, which entered service in 1989. The United States Air Force intends to keep the F-15 Eagle in service until the year 2025. The maneuverability of the F-15 derives from its low wing load (ratio between the weight and the wing area) with a high weight-to-weight ratio that allows you to make tight turns without losing speed. The F-15 can climb to 10,000 meters in about 60 seconds. The F-15E was designed for the ground attack but maintains the lethality in the air-to-air combat of the F-15 Eagle.

To increase its range, the F-15E is equipped under the wing inserts with two conformable fuel tanks (CFT) that anchored to the fuselage, produce less aerodynamic drag than conventional external fuel tanks that are anchored in the pylons under the fuselage and the wings. However, unlike conventional external fuel tanks, CFTs cannot be launched in flight. Therefore, the increase of the range has a cost in the performance of the airplane with respect to a totally “clean” configuration without external tanks, due to the additional weight and resistance that they suppose.

Technical specifications (F-15 Eagle)

– Crew: 1 pilot
– Maximum takeoff weight: 30,845 km / h
– Maximum operative speed: 2,660 km / h (Mach 2,5+)
– Speed at sea level: 1,450 km / h (Mach 1,2)
– Reach by ferry: 5,552 km with 2 fuel tanks and 3 external launchable tanks.
Action radius: 1,967 km
– Service ceiling: 19,812 m
– Ascent regime: 254 m / s

Conclusion

I hope you liked this section. If some you see you had any doubt and I hope we can discuss it all here on my blog. And know what you think every 1 with all this. Greetings.

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