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Sukhoi Design Bureau
Su-35 Flanker E/M/S

Type Multirole fighter, air superiority fighter
National origin Soviet Union (Russia since 1991)
Manufacturer United Aircraft Corporation (for Su-35S)
Designer Sukhoi Design Bureau
Built by Sukhoi
Status In service
Primary users Russian Aerospace ForcesPeople's Liberation Army Air Force
Algerian Air Force
Number built Su-27M: 12
Su-35S: >151
History
Manufactured Su-27M: 1987–1995Su-35S: 2007–present
Introduction date February 2014
First flight Su-27M: 28 June 1988; 37 years agoSu-35S: 19 February 2008; 17 years ago
Developed from Sukhoi Su-27
Variants Sukhoi Su-37

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History Sukhoi Design Bureau Сухой Су-35
Sukhoi Su-35 Flanker E/M/S



The Sukhoi Su-35 (Russian: Сухой Су-35; NATO reporting name: Flanker-E/M, occasionally nicknamed "Super Flanker" is the designation for two improved derivatives of the Su-27 air-defence fighter. They are single-seat, twin-engine, supermaneuverable, 4.5 generation 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.

Modernization

Thrust vectoring nozzle on a Sukhoi Su-35S

In many respects, the T-10BM design resembles the Su-27 more than the Su-27M. During tests of the thrust-vectoring engines and the Su-27M's aerodynamic layout, Sukhoi had concluded that the loss of manoeuvrability due to the removal of the canards – the addition of which imposed a weight penalty on the airframe – could be compensated for by the addition of thrust-vectoring nozzles. Industry progress in the fields of avionics and radars has also reduced the weight and size of such components, which shifts the centre of gravity of an aircraft rearward. Accordingly we saw SW, designers removed the canards (and the dorsal air brake) found on the Su-27M; the size of the vertical tails, aft-cockpit hump and tail boom were also reduced. With such changes, as well as the increased use of aluminium and titanium alloys and composites, designers had reduced the empty weight of the aircraft, while maintaining a similar maximum take-off weight to the Su-27M.

Su-35S cockpit layout: a head-up display, two multi-function liquid crystal displays, and a control stick with HOTAS controls
 

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Ceiling

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Combat RANGE

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Mach

Aircraft Speed

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Max Crew

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Voronezh Aircraft Production Association

Sukhoi Design Bureau Сухой Су-35
Sukhoi Su-35 Flanker E/M/S

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General Info

        • 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)
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Powerplant

    • mpty weight: 19,000 kg (41,888 lb)
    • 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 × Saturn AL-41F1S afterburning turbofan engines
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Performance

    • Maximum speed: 2,400 km/h (1,490 mph, 1,290 kn) at altitude
    • Maximum speed: Mach 2.25
      • 1,400 km/h (870 mph; 760 kn), Mach 1.13 at sea level
    • Cruise speed: 1,170 km/h (730 mph, 630 kn) / Mach 1.1+ supercruise at medium altitude
    • Combat range: 1,600 km (990 mi, 860 nmi) approx
    • Service ceiling: 18,000 m (59,000 ft)
    • g limits: +9
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Related development

    • Guns: 1 × internal 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds
    • Hardpoints: 12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations with a capacity of 8,000 kg 
Special Links Sukhoi Design Bureau Sukhoi Su-34 Fullback

Links to Youtube & Others

While the F-35’s combination of advanced stealth and sensor fusion, and AIM-9X missiles, makes it a strong performance at all ranges, the fighter is seriously hindered by one significant design shortcoming - namely an inability to deploy visual range missiles while in stealth configuration.

Sukhoi Design Bureau
Sukhoi Su-35 Flanker S

Should the F-35 carry AIM-9X missiles externally

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Youtube Link

While the F-35 has been much maligned for its limited flight performance, which is much more constrained than those of other fifth generation fighters.

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Read more in Sukhoi Design Bureau Sukhoi Su-34 Fullback

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