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Su-30

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

To fight the enemy cruise missiles Russian Air Force needed a double long-range fighter. The capacity of the combat capabilities of the Su-27 is clearly not enough. The bureau decided to use as the basis of double Su-27UB, production of which has been mastered at the Irkutsk aircraft plant. Work on the aircraft began in 1986 g. When testing the prototype Su-27UB it has worked out a system of refueling in the air. On the starboard, at the level of the canopy hood, It was installed L-shaped rod fuel consumer. On modernized "SPARK", known as the Su-27PU, It was also somewhat improved habitability conditions in the cockpit.

Su-30 – video

At the beginning 1987 g. the first flight of a converted "Spark" with a crew of test pilots and OKB. Votintsev and N. Sadovnikov. 23 June The nonstop flight T10U-2 with the same crew on the route Moscow - Komsomolsk-on-Amur - Moscow length 13 440 km and duration 15 no 42 min with four refueling. This has demonstrated the ability to use the upgraded Su-27UB as far interceptor. Aircraft refueling system received in the air, new navigation system, modernized system of remote control and weapons control.
The first of two pre-production aircraft Su-27PU (T10PW-5) flew on 31 December 1989 g. from the factory airfield Irkutsk Aviation Plant. Based on the results of flight tests of the modernized machine has begun mass production two-seat fighter, the designation Su-30. Externally Su-30 differed from the combat training Su-27UB presence retractable rod fuel consumer on the left side and right fairing offset head station optikolokatsionnoy. 14 April 1992 g. first flew the first production Su-30.

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

The Design Bureau jointly with IAPO created an export version of the Su-KRC ("K" - Commercial), received advanced capabilities in operations against ground targets. A further development was the Su-LOSC with advanced radar and greatly expanded the nomenclature of weapons. With its creation, used the experience of the development of the Su-35 fighter. Sioux LOSC designed to gain air superiority in theater, and destroy targets on land and at sea, the application of EW and firing of air defense countering, day and night, in all weather conditions. Work on the creation of the Su-LOSC started in 1991 city, and a prototype of the aircraft made its first flight 14 April 1992 g. (test pilots GE. Bulanov and VB. Maksimenkov). Externally, it practically does not differ from the Su-30. The rear cockpit is an indicator, which can be output video data from TV homing guided weapons. Su-LOSC has unique fighting abilities, putting it in first place among the world's production of heavy multirole fighters.

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

30 November 1996 g. Russian-Indian for the purchase contract has been signed 40 Su-30MKI (Indian - Index "AND"). 1 July 1997 g. The aircraft first flew on.
The plane formed by the aerodynamic configuration "longitudinal triplane", with thrust vector control system (UVT) engines, combined with a remote control system (CDS) by air, It provides a virtually unlimited maneuverability and unique characteristics runways. Radar can accompany both until 10 purposes and use missiles from two goals.

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

Tactic-technical characteristics of the Su-30

– First flight: 1989 year
– years of production: from 1992 of the year
– units produced: about 600 (on November 2017 of the year)

The cost of the Su-30

– $83 million (Indian Su-30MKI assemblies, 2012 year)
– $50 million (Su-30cm for the Russian Air Force, 2012 year)

Su-30 crew

– 2 man

The dimensions of the Su-30

– Length: 21,9 m
– Wingspan: 14,7 m
– Height: 6,36 m
– wing area: 62 m²
– Wing loading at normal takeoff weight: 398 kg / m
– The load on the wing at the maximum takeoff weight: 532 kg / m

All Su-30

– empty weight: 18800 kg
– Mass normal takeoff: 24900 kg
– Weight maximum takeoff: 34500 kg
– Mass limiting takeoff: 38800 kg
– fuel weight: 9640 kg

Engine Su-30

– 2 × TRDDF HE-31F ' (AL-31FP the Su-30SM)
– Maximum thrust besforsazhny: 2 × 7770 kgf
– Thrust in afterburner: 2 × 12500 kgf
– thrust vector deflection angles (for AL-31FP): ± 16 ° in any direction, ± 20 ° in the plane
– thrust vector deflection speed (for AL-31FP): 60from
– weight: 1520 kg

Maximum overload: +9 G

Su-30 speed

– Maximum speed at ground: 1350 kmh (M = 1.13)
– Maximum speed at height: 2 350 kmh (M = 1.9603 )

Range of flight of Su-30

– near the ground: 1270 km
– on high: 3000 km
– combat radius: 1500 km
– flight duration: 3,5 no (without refueling)

Practical ceiling Su-30

– 17300 m

takeoff speed SU 30

– 13800 m / min (230 m / s)
– The length of the run: 550 m
– path length: 750 m

Thrust-to-weight ratio of the Su-30

– during normal takeoff weight: 1,00
– at maximum takeoff weight: 0,84
– at the maximum take-off weight: 0,76

Weapon Su-30

– cannon: 30-Built-mm cannon GS-30-1
– point of suspension: 12
– combat load: 8000 kg (to 10,4 t on RLE).
– 6 medium-range missiles P-77, P-27R or P-27ЭR, P-P-27T or 27ET with TGS and 6 close combat rockets P-73 TGS;
– weight svobodnopadayuschie bombs 500 kg (to 8 units) or 250 kg (28 units);
– Containers EP-U (to 7 units) or blockage HAP C-13 and C-8 (to 4 units);
– Various combinations guided and unguided weapons of various classes.

Photo Su-30SM

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

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 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

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 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

 Su-30 Dimensions. Engine. The weight. story. Range of flight. Service ceiling

Rise Su-30MKI

 

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