Sukhoi Su-35 Multi-Role Fighter Aircraft : Go Defence News

Sukhoi Su-35 Sukhoi SU-27 is the designation for two separate, heavy-upgraded derivatives of Air Defense Combat Aircraft. These are single-seat, two engines, high-quality combat aircraft, which are designed by Sukhoi Design Bureau and have been created by the Komsomolsk-on-Amur Aircraft Production Association.
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The first version was prepared in the 1980s as the second edition of Sukhoi SU-27. And it was initially known as Sukhoi SU-27M. Multi-function radar was added to this version, which changed it from ordinary aircraft to multirol aircraft. And it was structurally reinforced to handle its weight. Its first prototype made its first flight in June 1988. Due to the collapse of the Soviet Union, the aircraft was not produced on a large scale. Sukhoi re-named the aircraft Sukhoi SU-35 to attract export orders. At the same time, fourteen planes were produced for tests and demonstrations. Thrust vectoring engines were installed in a prototype and as a result Sukhoi SU-37 was used as a technology demonstrator. At the end of 1990, the only Sukhoi SU-35 UB two-seat trainer aircraft was built which was built on Sukhoi SU-30MK family.

Sukhoi Su-57 Fifth generation jet fighter

In 2003, Sukhoi started the second modernization of Sukhoi SU-27 to serve as an interim aircraft due to the development time of Sukhoi SU-57. It is mainly known as Sukhoi SU-35. Thus Sukhoi SU-35 made its first flight in February 2008. Although the aircraft was designed for export, the launch of the Russian Air Force aircraft in 2009 became the customer, whose production version was named as Sukhoi SU-35S. People's Liberation Army of China (PLA)is the only foreign user of Air Force aircraft. In other countries, there has been a discussion about the purchase of Sukhoi SU-35 with Russia, which includes Indonesia, whose government is expected to sign a contract with Russia in the near future.

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Sukhoi SU-35-27M / SU-35

Single-seat fighter aircraft design with factory code of T-10M ("Upgraded"). In the first two prototypes, a new force was a fusel, canned and updated fly-by-wire flight-control system. Sukhoi SU-35-27M was operated by the AL-31FM turbofan engine. In 1995 two prototypes, nine pre-production and three production aircraft were made. Two stationary test aircraft were also built (T-10M-0 and T-10M-4). Due to the collapse of the Soviet Union, aircraft were not produced at large scale.

Sukhoi SU-37

Technology demonstrator was changed from the eleventh developmental Sukhoi SU-27M. Sukhoi SU-AL-31 FP engine with digital fly-by-wire flight control system, a glass cockpit, N 0011 M radar and thrust-vectoring nozzle was installed.

Sukhoi SU-35 UB

Two-seat trainer aircraft has been designed and made by the Komsomolsk-on-Amur Aircraft Production Association. The aircraft was powered by AL-31FP engines with thrust-vectoring nozzles. Although training aircraft, Sukhoi SU-35 UB was made to fight completely.

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Sukhoi SU-35 BM

Single-seat fighter aircraft, which is a new design of the original Sukhoi SU-27. The aircraft is powered by thrust-vectoring turbofan engines which are capable of supercruz. It is also known as T-10 BM.

Sukhoi SU-35S

According to Aviation Week and Space Technology, Sukhoi SU-35S is the designation of the T-10 BM design to be produced for the Russian Air Force.

Operators of  Sukhoi SU-35


Chinese Air Force ordered 24 Sukhoi SU-35S in 2015 was the first 4 aircraft were distributed At the end of December 4, 2016.


Russian Air Force - up to October 2017 in the 64 Sukhoi SU-35S service More than 50 planes were ordered in January 2016. The distribution rate will be 10 aircraft per year.

Specifications (SU-35)

General Detailes SU-35

Crew: 1
Length: 21.9 m (72 ft 11 in)
Wingspan: (with wingtip pods) 15.3 meters (50 feet 2 inch)
Height: 5.9 meters (19 feet 5 inches)
Feather area: 62 meters² (667 feet²)
Free weight: 18,400 kg (40,570 lb)
Useful load: 25,300 kilograms (56,660 lb) 50% on internal fuel
Maximum Flight Weight: 34,500 Kg (76,060 lb)
Fuel capacity: 11,500 kg (25,400 lb) interior
Power Plant: 2 × Sarton L-41 Afterburner Turbofan
Original thrust: 86.3 kilonauton (19,400 lb) by each
Thrust with Afterburner: 142 kilonautons (31,900 lb) from each

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Maximum speed:
At height: Mac 2.25 (2,400 km / hr; 1,490 mph)
At sea level: Mac 1.13 (1,400 km / h; 870 mph)
At elevation: 3,600 km (2,240 miles)
At sea level: 1,580 km (980 miles)
Ferry Range: 4,500 km (2,800 miles) with 2 external fuel tanks
Maximum service limit: 18,000 meters (59,100 feet)
Mounting rate:> 280 meters / second (> 55,000 feet / min)
Wing loading:
With 50% fuel: 408 kg / m² (84.9 lb / ft²)
With full internal fuel: 500.8 kg / m² ()
Thrust / weight: 1.13 with 50% fuel (0.92 with full internal fuel)
Maximum G-Load: + 9 g

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