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Sukhoi Su-35

The Sukhoi Su-35 (Russian: Сухой Су-35; NATO reporting name: Flanker-E/M) is the designation for two improved derivatives of the Su-27 air-defence fighter. They are single-seat, twin-engine, supermaneuverable air superiority fighters, designed by the Sukhoi Design Bureau and built by Sukhoi.

The type was originally developed by the Soviet Union from the Su-27 and was known as the Su-27M. It incorporated canards and a multi-function radar giving it multi-role capabilities. The first prototype made its maiden flight in June 1988. Following the dissolution of the Soviet Union Sukhoi re-designated it as the Su-35 to attract export orders. Fourteen aircraft were produced and used for tests and demonstrations; one example had thrust-vectoring engines and was in turn redesignated the Su-37. A sole Su-35UB two-seat trainer was also built in the late 1990s that resembled the Su-30MK family.


In 2003, Sukhoi embarked on a second "deep" modernization of the Su-27 to serve as an interim export aircraft awaiting the development of the Sukhoi PAK FA (Su-57) program. Also known as the Su-35, this version incorporates technology from the PAK FA program and has a redesigned cockpit and weapons-control system and features thrust-vectoring engines in place of the canards.[6] The type made its first flight in February 2008. Although it was designed for export, the Russian Air Force became the launch customer in 2009, with the production version designated Su-35S. China's People's Liberation Army Air Force has also placed orders.

Design and development[edit]

Upgraded Su-27[edit]

The first aircraft design to receive the Su-35 designation had its origins in the early 1980s, at a time when the Su-27 was being introduced into service with the Soviet Armed Forces. The definitive production version of the Su-27, which had the factory code of T-10S, started mass ("serial") production with the Komsomolsk-on-Amur Aircraft Production Association (KnAAPO) in 1983. The following year, this Su-27 version reached initial operational readiness with the Soviet Air Defence Forces.[7] Having begun work on an upgraded Su-27 variant in 1982,[8] the Sukhoi Design Bureau was instructed in December 1983 by the Soviet Council of Ministers to use the Su-27 as the basis for the development of the Su-27M (T-10M).[9] Nikolay Nikitin would lead the design effort throughout much of the project's existence, under the oversight of General Director Mikhail Simonov, who had been the chief designer of the Su-27[10] along with Mikhail Pogosyan.

Operational history[edit]

Russia[edit]

In 1996, three production Su-27Ms were delivered to the air force's 929th State Flight Test Centre named for V. P. Chkalov (GLITs) at Vladimirovka air base, Akhtubinsk, to perform weapons trials.[21] In 2001, the air force decided to transfer several Su-27Ms to re-equip the Russian Knights aerobatics team, and so the team's pilots took familiarisation flights with the aircraft.[74] The three production and two other pre-production Su-27Ms arrived at the team's Kubinka air base near Moscow in 2003. However, they were used as a source of spare parts for other aircraft in the demonstration fleet.[75]

People's Liberation Army Air Force

[3]

Notable accidents[edit]

The fourth Su-35BM prototype was destroyed in a high-speed taxi run on 26 April 2009 due to brake failure. The aircraft crashed into the barrier at the end of the runway and was destroyed. The pilot ejected and sustained burn injuries.[59]


On 31 July 2021, a Su-35S fighter crashed after suffering an engine failure during a routine training mission in the Khabarovsk Territory in Russia, according to statement from the Russian Defence Ministry.[239] According to a preliminary investigation reported by the Russian newspaper Top War, the Su-35 suffered technical malfunctions in the environment control systems that indicate heating and cooling functions.


On 28 March 2024, a Su-35 crashed into the sea off Sevastopol. The pilot is reported to have safely ejected.[240]

Crew: 1

Length: 21.9 m (71 ft 10 in)

Wingspan: 15.3 m (50 ft 2 in)

Height: 5.9 m (19 ft 4 in)

Wing area: 62 m2 (670 sq ft)

: 5%

Airfoil

Empty weight: 19,000 kg (41,888 lb)

[243]

Gross weight: 25,300 kg (55,777 lb) with 50% internal fuel

Max takeoff weight: 34,500 kg (76,059 lb)

Fuel capacity: 11,500 kg (25,400 lb) internal

Powerplant: 2 × afterburning turbofan engines, 86.3 kN (19,400 lbf) thrust each dry, 137.3 kN (30,900 lbf) with afterburner, 142.2 kN (32,000 lbf) in emergency power

Saturn AL-41F1S

Data from KnAAPO,[44][241] Jane's All The World's Aircraft 2013[242]


General characteristics


Performance


Armament



Avionics

Sukhoi Su-27

Sukhoi Su-30

Sukhoi Su-33

Sukhoi Su-34

Sukhoi Su-37

[N 2]

Sukhoi Su-57

Related development


Aircraft of comparable role, configuration, and era


Related lists

KnAAPO

Rosoboronexport