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The Su 30 MKI is a customized Su 27 PU (ASCC codename:  Flanker) built according to Indian specifications. The M is for Modernized, K for Commercial and I for Indiski (India). It is probably the first time that an aircraft has been built in Russia for a foreign customer specifications.

The Su 30 was evaluated along-with the Mirage 2000-5, and found to be cheaper, hence was chosen.


The Su 27 was first evaluated by the IAF in 1994, when a team led by the CAS (ACM S.K.Kaul) in Russia.

The contract for the first 40 Su 30 fighters was signed in 1996, and the aircraft originally supposed to be delivered in batches and in a phased manner from 1997 through till 2000, with each batch being progressively more improved that the previous batch.

In 1998, the IAF signed another contract for the delivery of a further 10 aircraft, originally scheduled to be delivered to Indonesia.

In October of 2000, a Memorandum of Understanding was signed, which paved the  way for a complete Transfer of Technology and the manufacture of a further 140 Su 30 MKIs in India by the Hindustan Aeronautics Limited(HAL). The deliveries were not with out their delays, which were flayed in the India media, however, the first batch of Su 30 MKIs were delivered in mid 2002 to the Lohegaon AFB in Pune.


There are now 2 squadrons, the No 24 Hunting Hawks with the Su 30 MKs and the No. 20

Lightnings with the Su 30 MKIs. The full spec Su 30 MKI is however not delivered, with a few software updates remaining.







Physical Dimensions:

Length: 21.9 mts

Span: 14.7 mts

Height: 6.4 mts



Take Off weights

Normal: 24,900 kgs

Maximum: 34,500 kgs


Service ceiling: 17.3 kms




On internal fuel only: 3000 kms

With on mid-air refueling: 5200 kms


G limits: +9/ -?


Climb rate: 45,300 feet/min




At sea-level: 1350 kmph

At 11,000 mts: Mach 2+




Su 30 K/ Su 30 MK: 2, Al 31F Turbofans, each rated at 27,500 lbs, full afterburner thrust


Su 30 MKI: 2, Al 31FP Turbofans, each rated at 29,400 lbs full afterburner thrust. The Al 31 FPs has thrust vectoring nozzles. The nozzles are capable of deflecting 32 degrees in the horizontal plane and 15 degrees in the vertical plane.


The engines reportedly have an MTBO of ~1000 hours, while the TV nozzles have an MTBO of ~250 hours.

 Su 30 MKIs also can use the Mk 32.B buddy-buddy refueling pods.





The crew are provided zero-zero KD-36DM ejection seats which have a slightly modified communication/oxygen interface block compared to the earlier Su-27 blocks. Rear seat is raised for better visibility. The cockpit will be provided with containers to store food and water reserves, a waste disposal system and increased amounts of oxygen. The KD-36DM ejection seat is inclined at 30.


The French company Sextant Avionique will supply six liquid colour displays, five MFD 55s and one MFD 66, for both the pilot and his WSO (Weapons System Officer), the Totem inertial guidance system (dual-INS) with the GPS technology and the VEH 3000 holographic HUD. 


The pilot also has the Gzarkhov 45A HMS (Helmet Mounted Sight) unit, which can guide the R 73s and the R60 MKs.





The Su 30 MKI is a twin-finned aircraft. The airframe is constructed of titanium and high-strength aluminium alloys. The engine nacelles are fitted with trouser fairings to provide a continuous streamlined profile between the nacelles and the tail beams. The central beam section between the engine nacelles consists of the equipment compartment, fuel tank and the brake parachute container. The fuselage head is of semi-monocoque construction and includes the cockpit, radar compartments and the avionics bay. Su 30 MKIs also have a high percentage of composites used in the air-frame.


 Stability and control are assured by a digital FBW. The canard notably assists in controlling the aircraft at large angles of attack (AoA) and bringing it to a level flight condition.






Avionics: The main sensor on the Su 30 MKI is the N011M Phased Array radar. It is a multi-mode dual frequency (X- and L-band channels, NATO I and D band) radar. It detects targets using a Non Co-operative Targeting method. It is designed to detect fighter-sized targets at 150-160 kms range, and can track 20 targets, while engaging 8.  It is capable of interleaving air-to-air and air-to-ground modes. In an air-to-ground mode, it can acquire surface targets at ranges of up to 200 km (and for large resolution targets, upto 400 kms) and provide ground-mapping, terrain-following, and terrain-avoidance functions. Small ground targets, like tanks, could be detected out to 40-50 km.


AA Modes: Velocity Search, Range While Search, Track While Scan, target ID, close combat modes.


AS Modes: Real beam mapping, DBS mapping, SAR mapping, moving ground target selection, tracking and measuring of ground target coordinates.


Anti shipping modes: Sea surface search, moving sea targets selection, tracking and measuring of sea target coordinates, sea target ID.

Antenna diameter is 1m, antenna gain 36dB, the main side lobe level is -25dB, average side lobe level is -48dB, beam width is 2.4 deg with 12 distinct beam shapes. The antenna weighs 100-110kg. It is both mechanically and electronically scanned to give increased field of view over a fixed phased array antenna.

The Bars radar uses an Indian Radar controller, under the Project Vetrivale (Lance of Victory). The project also has developed the mission computer and the display processors for the aircraft.


The radar can also serve as a command post for other aircraft, with target coordinates being automatically transferred to at least four other aircraft using a secure data link.


The aircraft has an opto-electronic surveillance & targeting system which consists of an IR direction finder, laser rangefinder and helmet mounted sight system. The OLS-30M, developed by UOMZ company has a vibration-proof receiver, micro-cryogenic system, improved service life and new software, with respect to the earlier OLS-27. Range is claimed to be 90km in pursuit and 40km head-on.


The communications equipment comprises VHF and HF radio sets, a secured digital telecommunications system, and antenna-feeder assembly. It mounts an automatic noise-proof target data exchange system, which provides for coordination of the actions of several fighter aircraft engaged in a group air combat. It is under the INCOM series, by HAL.


Self Defense:


The self-defence suite incorporates a newly developed accurate Radar Warning Receiver (RWR), called the Tarang Mk. II. The Su 30 MKI incorporates a number of chaff/ flare dispensers and active jammers. The Tarang system is a modified version of that fitted to the MiG 21 Bison. The Tarang was also developed under the Project Vetrivale.




Weapons capabilities:


Maximum External load: 8000 kgs.


Internal gun:


GSh-301, 30 mm, single barrel gun with a capacity of 170 rounds. Normally however, only 150 rounds are loaded. The gun is said to be very accurate and has a high rate of fire of 1500-1800 rounds per minute. Range against ground and air targets is 200-800 mts and 1200-1800 mts respectively.




The Su 30 MKI has 12 hardpoints for carrying various weapons, including air-to-air and air-to ground munitions. This can be increased to 14 using multiple ejector racks.



Air To Air Missiles:


R 77/ RVV-AE Upto 6 (Range: Head-On 100 kms, ARH)

R 27 RE1/ TE1/ EP Upto 6 (Range: Head-On 70-130 kms, SARH/ IR/ Passive)

R 73 RDM1/2 Upto 6 (Range: 30 kms, IR)



Air-To Ground missiles:


Kh 29 L/T Upto 6 (Range: 30/ 12 kms, Laser/ TV)

Kh 31 A/P Upto 6 (Range: 70 kms, Active/ Passive)

Kh 59 M Upto 2 (Range 200 kms, Active)



Guided Munitions:


KAB 500 KR/ 1500 KR Upto 6           

KAB 250L/500L Upto 3


Unguided  Munitions:


FAB 500T Upto 8

FAB/ OFAB 100-120/ 250-270 28

RBK 500 Upto 8

S 80M/ S 8MB Upto 80 pcs

S 25 OFM-PU Upto 4 pcs






Discussions on the ACIG forum (www.acig.org )


Vayu Aerospace Review




www.bharat-rakshak.coms IAF page (http://www.bharat-rakshak.com/IAF/Aircraft/Specs/index.html )


Vayu-Senas Su 30 MKI info page (http://vayu-sena.tripod.com/info-su30mki.html#5