Sukhoi Su-35

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Su-35
Type Multirole fighter
Manufacturer Sukhoi
Designed by Mikhail Simonov
Maiden flight May 1985
Status Production
Primary user Russian Federation Air Force
Unit cost US $35 million

The Sukhoi Su-35 (NATO designation: Flanker-E) is an advanced fighter aircraft in the Russian Federation Air Force inventory.

A development of the Su-27, it was originally identified as the Su-27M. It was developed to counter the US F-15 Eagle and F-16 Fighting Falcon.

Following flight tests from 1988, based on the 1985 experimental T10-24, the first prototype was publicly displayed in 1992 at the Farnborough Air Show. Flight testing continued and up to 1994 eleven prototypes were built. Intended to enter service around 1995, the first test flights of an improved Su-35, the Su-37, in 1996 and the transfer of existing Su-35 prototypes to this program appeared to suggest the end of the Su-35, but later the Su-37 aircraft were converted to Su-35 back again, and it's in production for selected units of the Russian Air Force. It shares much in common with the naval variant of the Su-27, the Su-33, notably the larger wings and the more powerful engines. Other changes from the Su-27 were canards, a larger nose, the greater use of carbon fibre and aluminium-lithium alloy in the airframe, and larger, squarer tail fins. The new nose holds an improved radar and the aircraft had many other upgrades to its avionics and electronic systems, including digital fly-by-wire and a rear-looking radar for firing Semi-Active Radar missiles.

A two-dimensional asymmetric thrust vectoring system was tested on the Su-35 and seems to be the basis for the development of the Su-37. A new type of 2D thrust vectoring engine, the 117S, is planned to replace the current AL-35.[1]

11 are in use in the Russian Air Force.

[edit] Specifications (Su-35)

General characteristics

  • Crew: One
  • Length: 22.20 m (72.83 ft)
  • Wingspan: 15.15 m (49.70 ft)
  • Height: 6.43 m (21.08 ft)
  • Wing area: 62.0 m² (666 ft²)
  • Empty weight: 17,500 kg (38,600 lb)
  • Loaded weight: 25,700 kg (56,660 lb)
  • Max takeoff weight: 34,000 kg (74,995 lb)
  • Powerplant: 2× Lyulka AL-35MF turbofans, 137 kN (30,800 lbf) each

Performance

Armament

[edit] Related content

Related development

Comparable aircraft

Designation sequence

Related lists

See also


[edit] External links