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Sukhoi Su-30

Military Aircraft

The Sukhoi Su-30, NATO reporting names Flanker-C, G and H, is a twin-engine, two-seat supermaneuverable multirole fighter of the Su-27 family, meant for all-weather air-to-air and interdiction missions. It began as an internal Sukhoi project that took the Su-27UB two-seat trainer as the basis for the Su-27PU interceptor, which the Russian Defence Ministry renamed Su-30 in 1996; a proof-of-concept demonstrator flew on 6 June 1987. Different export requirements later split the type into two branches built by competing organisations, KnAAPO's Su-30MKK and Su-30MK2 for China and other buyers, and Irkut's Su-30MKI for India. The Russian Aerospace Forces were reported to have 130 Su-30SMs in operation as of 2024.

Facts
Year
1987 1
Engine Class
Jet 1
Status
In service 1
Top Speed (km/h)
2120 1
Mass (kg)
17,700 1
Maximum Mass (kg)
34,500 1
Comparison
Body Style
Aircraft (no road body style) 1
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Aviation, Modes
Source Sukhoi Su-30 (Wikipedia)

Of Make

Source Sukhoi Su-30 (Wikipedia)
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Source Sukhoi Su-30 (Wikipedia)Lead, body style
Quote, Lead, body style
is a twin-engine, two-seat supermaneuverable fighter aircraft developed in the Soviet Union in the 1980s by Russia's Sukhoi Aviation Corporation.

Originated In

Also in Geography Atlas: where this subject originated.

Source Sukhoi Su-30 (Wikipedia)Lead, body style
Quote, Lead, body style
is a twin-engine, two-seat supermaneuverable fighter aircraft developed in the Soviet Union in the 1980s by Russia's Sukhoi Aviation Corporation.
Sources
1. Sukhoi Su-30 (Wikipedia)
  • Development
    A "proof-of-concept" demonstrator flew on 6 June 1987
  • Lead
    The Russian Aerospace Forces (VKS) were reported to have 130 Su-30SMs in operation as of 2024.
  • Specifications
    Powerplant: 2 × Saturn AL-31FL/FP Afterburning turbofan engines, 74.5 kN (16,700 lbf) thrust each dry
  • Lead, body style
    is a twin-engine, two-seat supermaneuverable fighter aircraft developed in the Soviet Union in the 1980s by Russia's Sukhoi Aviation Corporation.
  • Specifications, maximum speed
    Maximum speed: 2,120 km/h (1,320 mph, 1,140 kn) at high altitude
  • Specifications, empty weight
    Empty weight: 17,700 kg (39,022 lb)
  • Specifications, maximum takeoff weight
    Max takeoff weight: 34,500 kg (76,059 lb)
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