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The Pilots Desk
Fightersmulti-role combat aircraft version of the Su-30 fighter aircraft

Sukhoi Su-30

Sukhoi Su-30

The Sukhoi Su-30 (Russian: Сухой Су-30; NATO reporting name: Flanker-C/G/H) is a twin-engine, two-seat supermaneuverable fighter aircraft developed in the Soviet Union in the 1980s by Russia's Sukhoi Aviation Corporation. It is a multirole fighter for all-weather, air-to-air interdiction missions. The Russian Aerospace Forces (VKS) were reported to have 130 Su-30SMs in operation as of 2024. The Su-30 started as an internal development project in the Sukhoi Su-27 family by Sukhoi. From the Su-27UB two-seat trainer, the Su-27PU heavy interceptor was developed. The design plan was revamped and the Su-27PU was renamed to Su-30 by the Russian Defense Ministry in 1996. Of the Flanker family, the Su-27, Su-30, Su-33, Su-34 and Su-35 have been ordered into limited or serial production by the Russian Defense Ministry. Later, different export requirements split the Su-30 into two distinct version branches, manufactured by competing organizations: KnAAPO and the Irkut Corporation, both of which come under the Sukhoi aerospace group's umbrella. KnAAPO manufactures the Su-30MKK and the Su-30MK2, which were designed for and sold to China, and later Indonesia, Uganda, Venezuela, and Vietnam. Due to KnAAPO's involvement from the early stages of developing the Su-35, these are basically a two-seat version of the mid-1990s Su-35. The Chinese chose an older but lighter radar so the canards could be omitted in return for increased payload. It is a fighter with both air supremacy and attack capabilities, generally similar to the U.S. F-15E Strike Eagle. Irkut traditionally served the Soviet Air Defense and, in the early years of Flanker development, was responsible for manufacturing the Su-27UB, the two-seat trainer version. When India showed an interest in the Su-30, Irkut offered the multirole Su-30MKI, which originated as the Su-27UB modified with avionics appropriate for fighters. Along with its ground-attack capabilities, the series adds features for the air-superiority role, such

Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.

Category
Fighters
First flight
1989-12-31
Length
21.935 m
Wingspan
14.7 m

Specifications

Max speed
614 kt
Range
1,600 nm
Service ceiling
56,800 ft
Rate of climb
45,000 ft/min
Max takeoff weight
76,059 lb
Empty weight
39,022 lb
Fuel capacity
9.3 US gal
Powerplant
2 × Saturn AL-31 FL/FP Afterburning turbofan engines
Engines
2
Seats
2
Length
72 ft
Wingspan
48 ft
Height
21 ft
Number built
630

Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).

Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.