The Sukhoi Su-35 designation covers two improved derivatives of the Su-27 air superiority fighter, both single-seat, twin-engine, supermaneuverable 4.5 generation fighters from the Sukhoi Design Bureau. The first, known at the time as the Su-27M, added canards and a multifunction radar, made its maiden flight in June 1988 and was relabelled Su-35 after the Soviet collapse in the hope of export orders; fourteen were built for tests and demonstrations. The second, a deep modernisation begun in 2003 that uses thrust-vectoring engines in place of canards and technology from the PAK FA programme, first flew in February 2008. The Russian Air Force became its launch customer in 2009 with the Su-35S, and the Chinese military received its first four aircraft in December 2016.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Sukhoi Su-35 (Wikipedia)
Of Make
Source Sukhoi Su-35 (Wikipedia)
Sources
1. Sukhoi Su-35 (Wikipedia)
Lead
The type made its first flight in February 2008.
Lead, Su-27M prototype
The first prototype made its maiden flight in June 1988.
Specifications
Powerplant: 2 × Saturn AL-41F1S afterburning turbofan engines, 86.3 kN (19,400 lbf) thrust each dry
Lead, body style
They are single-seat, twin-engine, supermaneuverable, 4.5 generation air superiority fighters, designed by the Sukhoi Design Bureau and built by Sukhoi.
Specifications, maximum speed
Maximum speed: 2,400 km/h (1,490 mph, 1,290 kn) at altitude
Specifications, empty weight
Empty weight: 19,000 kg (41,888 lb)
Specifications, maximum takeoff weight
Max takeoff weight: 34,500 kg (76,059 lb)
Lead, country of origin
The type was originally developed by the Soviet Union from the Su-27 and was known as the Su-27M.
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