Su-30MKI

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Su-30MKI

Su-30MKIs in Service with the Indian Air Force
Type	Air Superiority fighter, MultiRole Fighter, Strike fighter, Heavy class fighter
Manufacturer	Sukhoi
Maiden flight	1989
Introduced	1996
Status	in Active Service
Primary user	Indian Air Force
Number built	190
Unit cost	US$33-$45 million

Sukhoi Su-30 MKI, (Russian: Modernizirovannyi Kommercheskiy Indiski; Modernized Commercial India), is the variant of the Sukhoi Su-30. The Su-30 MKI a highly specialized aircraft developed for the Indian Air Force. It is a heavy class, long-range, multi-role, air superiority fighter and strike fighter. The variant also consists of French, Israeli and Indian subsystems. The MKI variant is a much more advanced fighter jet than the basic K and MK variants and is considered a 4.5 generation aircraft. The MKI variant is considered to be the most advanced fighter aircraft of Russian origin in service, except for Su-35.

[edit] Su-30 MKI overview

The MKI version is the ultimate development of the Su-30 series, and regarded as superior in capabilities to all versions of F-15 aircraft of the USAF. Though a variant of Su-30, the Su-30 MKI is significantly more advanced than the basic Su-30 or the Chinese Su-30 MKK aircraft. This variant has significant upgrades on it from the basic Su-30 MK version. The aircraft was jointly designed by Russia's Sukhoi and India's HAL.
India exercised its Su-30 MKIs against the Royal Air Force's Tornado ADVs in October 2006 ^[1] This marked the first large scale exercise with any foreign Air Force, in which the IAF used its MKI's extensively. This exercise was also the first in 43 years with the Royal Air Force.

Deadliest formation in world!
Two IAF Su-30 MK (rear) and two USAF F-15 Eagles fly with two IAF Mirage 2000 (middle of V-formation) during Cope India '04

[edit] Improvements

Canard Foreplanes:Canards are installed to increase lifting effectiveness and enhance manoeuvrability of the aircraft, They are deflected automatically to ensure controllable flight at high angles-of-attack.
Thrust Vectoring Control: The 2D TVC makes an aircraft highly maneuverable. The aircraft is capable of near-zero airspeed at high angles of attack and dynamic aerobatics in negative speeds up to 200 km/h.
The N011-M Bars phased array Radar.
A multi-national Avionics complex sourced from Russia, France,Israel and India which include Display, Navigation, Targeting and Electronic warfare systems.

More than 40 Su-30 MKI aircraft are currently serving in the IAF, and belong to different batches- Mk.1, Mk.2 and Mk.3.

190 Su-30 MKIs, of Mk.3 standards and beyond, are expected to be in service by 2012.

[edit] MKI Comparison with other Su-30 variants

The Su-30 MKI has a maximum range, with one in-flight refuelling, of 8000 km. The Su-30MK and Su-30MK-1 have a maximum range, with one in-flight refuelling, of 5200 km (35% less than MKI variant).
The Su-30MKI has thrust vectoring engines whereas the Su-30MK and Su-30MK-1 do not have thrust vectoring engines.
The maximum speed of the MKI is higher than other variants.
The radar range & detection is further and more sensitive than other variants.
MKI can track and engage more enemy targets simultaneously than other variants

[edit] Purchase

After 2 years of evaluation and negotiations, in 1996, India decided to purchase Su-30 aircraft.

India signed a US $1.462 billion deal with Sukhoi on 30 November 1996 for the delivery of 40 Su-30 aircraft. These aircraft were to be delivered in three batches. The first batch were 10 Su-30K or Su-30MK, the basic version of Su-30. The second batch were to be 8 Su-30MK with French and Israeli avionics. The third batch were to be 10 Su-30MKs featuring carnard foreplanes. The fourth and final batch Su-30MKIs of 12 aircraft were to have the AL-31FP turbofans.
After the delivery of the first batch, the second batch was delayed for unknown reasons. Thus it was decided to take delivery of full-standard Su-30MKIs.
IAF decided to buy 10 additional Su-30Ks which were originally destined for Indonesia.
The first batch of 8 Su-30Ks and these 10 additional Su-30Ks were to upgraded in India by HAL.

In 2000, an agreement was signed allowing the license production of 140 Su-30MKIs in India. The deal was sealed in Russia at the IAPO factory. The deal combines license production with full technology transfer and hence called a 'Deep License'.
India will eventually acquire a total of 190 Su-30MKI. Out of these 50 will be made in Russia while the rest will be produced in India by Hindustan Aeronotics Limited (HAL).
Recent news indicates that Belarus is to buy the second hand 18 Su-30Ks from India ^[2] Though a variant of Su-30, the Su-30 MKI is significantly more advanced than the Su-30MK or the Chinese Su-30 MKK variants.
IAF recently wants to aqcuire 40 Su-30MKI from Russia due to reduction in force levels.

[edit] Technical information

[edit] Airframe

The Su-30MKI is a highly integrated 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 fins and horizontal tail consoles are attached to 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.

[edit] Aerodynamics

Su-30MKI aerodynamic configuration is an unstable longitudinal triplane. The canard increases the aircraft lifting and deflects automatically to allow high angle-of-attack flights.
The integral aerodynamic configuration combined with thrust vectoring results in practically unlimited manoeuvrability and unique taking off and landing characteristics.
The Su-30MKI has no level winged AoA limitations: it can fly at even 180 degree AoA and still recover. This high super-agility allows rapid deployment of weapons in any direction as desired by the crew.
The canard notably assists in controlling the aircraft at large angles of attack (AoA) and bringing it to a level flight condition. The wing will have high-lift devices featured as deflecting leading edges and flaperons acting the flaps and ailerons.

[edit] Further information

[edit] Flight control

The aircraft has a Fly By Wire with quadruple redundancy. Depending on the flight conditions, signals from the control stick position transmitter or the FCS will be coupled to the remote control amplifiers. These signals are combined with feedback signals fed by acceleration sensors and rate gyros.
The resultant control signals are coupled to the high-speed electro-hydraulic actuators of the stabilizers, rudders and the canard. The output signals are compared and, if the difference is significant, the faulty channel is disconnected.
FBW is based on a stall warning and barrier mechanism which prevents development of aircraft stalls through a dramatic increase in the control stick pressure. This allows a pilot to effectively control the aircraft without running the risk of reaching the limit values of AoA and acceleration

[edit] Cockpit instrumentation

The displays include an Elbit Su 967 head up display and seven liquid crystal multifunction displays, six 127 mm x 127 mm and one 152 mm x 152 mm. The HUD was widely misreported to be the VEH 3000 from Thales but is from Elbit instead. Variants of the same HUD have also been chosen for the IAF's MiG-27 and SEPECAT Jaguar upgrades, on grounds of standardisation. Flight information is displayed on four LCD displays which include one for piloting and navigation, a tactical situation indicator, and two for display systems information including operating modes and overall operation status. The rear cockpit is fitted with a larger monochromatic screen display for the air-to-surface missile guidance

[edit] Navigation

The aircraft is fitted with a satellite navigation system (A-737 GPS compatible), which permits it to make flights in all weathers; day and night. The navigation complex comprises of high accuracy Sagem integrated global positioning system and ring laser gyroscope inertial navigation system.

[edit] Communication

The communications equipment comprises secure VHF and HF radio sets, a secured digital telecommunications system, and antenna-feeder assembly. It mounts a noise-proof target data exchange system, which provides for coordination of the actions of several fighter aircraft engaged in a group air combat. An automatic flight control system makes all phases of its flight automatic, including the combat employment of its weapons.

[edit] Two-pilot crew

Two-pilot crew provides higher work efficiency as well as the engagement in close and long range combats and the air situation observation. Besides, the same dual control aircraft can be used as a combat and training aircraft. Additionally, the integrated air-borne equipment enables the aircraft to be used as an air command post to control the operation of other aircraft.
The back seater is WSO (Weapons Systems Operator). The pilot flies the aircraft and handles air-to-air and some ATG weapons, as well as countermeasures. The WSO takes care of the detailed aspects of navigation, ground radar mapping & target designation, delivery solution for ATG weapons etc.

[edit] Ejection seats

The crew are provided zero-zero KD-36DM ejection seats. 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 30º, to help the pilot resist aircraft accelerations in air combat.

[edit] Radar

The forward facing NIIP NO11M Bars (Panther) is a powerful integrated passive electronically scanned phased array radar. The N011M is a digital multi-mode dual frequency band radar.

Features:

The N011M can function both in air-to-air and air-to-land/sea mode simultaneusly while being tied into a high-precision laser-inertial or GPS navigation system. It is equipped with a modern digital weapons control system as well as anti-jamming features.
For aircraft N011M has a 350 km search range and a maximum 200 km tracking range, and 60 km in the rear hemisphere. A MiG-21, for instance can be detected at a distance of up to 135 km. Design maximum search range for an F-16 target was 140–160 km.
The radar can track 20 air targets and process engage the 8 most threatening targets simultaneously and attack 4 most dangerous simultaneously^[3] These targets include from cruise missiles to even motionless helicopters.

Irkuts press release on the Su-30 MKI Mk3.
The Su-30MKI can function as a 'mini-AWACS' and can act as a director or command post for other aircraft. The target co-ordinates can be transferred automatically to at least 4 other aircraft.
The radar can detect ground targets such as tanks at 40- 50 km.
The N011M is claimed to detect large sea targets at a distance up to 400 km, and small sized ones at a distance of 120 km.

When integrated with the Brahmos Missile, the Su-30MKI could become a formidable anti-shipping platform.

Future upgrades:

Future upgrade plans include new gimbals for the antenna mount to increase the field of view to about 90-100 degrees to both sides. New software will enable a Doppler-sharpening mode and the capability to engage up to eight air targets simultaneously.
By 2010, when the first totally-built Su-30MKI will roll out from HAL, it could be equipped with a new phased array radar called the Irbis (Snow Leopard), which will replace the N011M Bars. These reports are yet to be confirmed by the Indian Air Force or official sources. The Irbis has been widely misreported to be an active phased array. It is not. NIIP in Vzlet, 2006 (a journal edited by noted aviation journalist A. Fomin) details the Irbis as a high power Passive electronically scanned array, built using the experience of the Bars project. However, it will have a lighter antenna derived from the NIIP Osa (Wasp) radar, new servos to rotate the antenna in both axes, with a greater field of regard (adding up to a total of 100 degrees), and an entirely new architecture with dual travelling wave tubes, giving a range of 400 km against a 3 meter square target (RCS). Using new high speed computers, the Irbis will be able to track 30 targets and engage 8. It will also be KS-172 capable.

Radar modes:

Air-to-Air : velocity search, range while search, track while scan, target ID, close combat modes.
Air-to-Surface : Real beam mapping, DBS mapping, SAR mapping, moving ground target selection, tracking and measuring of ground target coordinates.
Anti-shipping : Sea surface search, moving sea targets selection, tracking and measuring of sea target coordinates, sea target ID.

[edit] Weapons-related avionics

[edit] Laser-optical locator system

OLS-27 laser-optical locator system to include a day and night FLIR capability and is used in conjunction with the helmet mounted sighting system. The OLS-27 (Izdeliye 36Sh) is a combined IRST/LR device using a cooled, broader waveband, sensor.
Tracking rate is over 25 deg/s with 50 km range in pursuit engagement, 15 km head-on. The laser rangefinder operates between 300 and 3000 m for air targets, 300 and 5000 m for ground targets.
Detection range is up to 50 km, whilst the laser ranger is effective from 300 to 3000 m. Azimuth tracking is accurate to 5 s, whilst range data is accurate to 10 m. Targets are displayed on the same CRT display as the radar. Weighs 174 kg.

[edit] Targeting Pod

Israeli LITENING targeting pod will be used to target the laser guided munitions. Litening incorporates in a single pod all the targeting features required by a modern strike fighter.
The original pod included a 1st Generation FLIR, a TV camera, a flash-lamp powered laser designator, laser spot tracker for tracking target designated by other aircraft or from the ground, and an electro-optical point and inertial tracker, which enabled continuous engagement of the target even when the target is partly obscured by clouds or countermeasures.
The pod integrates the necessary laser rangefinder and designator, required for the delivery of Laser Guided Bombs, cluster and general purpose bombs.

[edit] Electronic countermeasures

An integrated ECM system turns on the warning units that provide signals about incoming enemy missiles, a new generation radio recon set, active jamming facilities and radar and heat decoys. It also includes an electronic intelligence unit, a chaff and flare dispenser and a RWR system.

The RWR system is an indigenously developed system by DRDO, called Tarang, (Spectrum in Sanskrit). It has direction finding capability and is known to have a programmable threat library. The RWR is derived from work done on an earlier system for India's MiG-23BNs known as the Tranquil, which is now superseded by the more advanced Tarang series.
Elta EL/M-8222 a self-protection jammer developed by Israel Aircraft Industries is the MKI's standard EW pod, which the Israeli Air Force uses on its F-15s. The ELTA El/M-8222 Self Protection Pod is a power-managed jammer, air-cooled system with an ESM receiver integrated into the pod. The pod contains an antenna on the forward and aft ends, which receive the hostile RF signal and after processing deliver the appropriate response.

[edit] Indian contribution

Su-30MKI is fitted with several Indian designed and manufactured avionic items. Several critical items were developed by DRDO under a project code named "Vetrivel" (Victory Vel in Tamil) in close collaboration with the PSUs and the IAF. These included the Mission computer, display processor and radar computer. Other systems supplied by the DRDO and HAL India include the INCOM frequency hopping, jam resistant radio set, radar altimeters, IFF units, as well as dial-pointer instrumentation for the cockpit, intended as a backup for the digital Liquid crystal displays.

Some of the components developed by Indian agencies were:

Mission Computer cum Display Processor-MC-486 and DP-30MK (Defence Avionics Research Establishment DARE): The 32-bit mission computer performs mission-oriented computations, flight management, reconfiguration-cum-redundancy management and in-flight systems self-tests. In compliance with MIL-STD-1521 and 2167A standards, Ada language was adopted for the mission computer's software.
Radar Computer - RC1 and RC2 (DARE)
Tarang Mk2 Radar Warning Receiver + High Accuracy Direction Finding Module
IFF-1410A - Identification Friend or Foe
Integrated communication suite
Radar altimeter

Other critical items from the Indian side, included test instrumentation and support equipment for the Sukhoi, which India now hopes to provide to other Sukhoi customers such as Malaysia.

Furthermore, Indian pilots and technical personnel played a vital role in optimizing the Sukhoi-30 MKI's ergonomics as well as information displays. Given the high level of user involvement, and local aeronautical expertise built up via the LCA program, it can be reasonably expected that Indian Su-30 MKI's will continue to evolve further.

[edit] Further developments in local avionics

The DRDO has gone a step further and come out with a new design of the Core Avionics Computer (CAC) which can be used with a single module adaptation across many other aircraft platforms.
The CAC which is derived from the computers designed for the Su-30MKI can also be also used in the avionics upgrades for the MiG-27 and Jaguar aircraft. The CAC was demonstrated by DRDO at the Aero India exhibition at Yelahanka and attracted a good deal of international attention. It has been suggested that a variant of the CAC may be also retrofitted to the Su-30 MKI. The advantage of the CAC is in its compact design, which performs both mission computing and display processing functions. DARE took up the development and delivery in quantities of Mission Computers, Display Processors and Radar Computers for the Su 30 avionics upgrade. The requirements were analysed and instead of building three different computers DARE developed nine functional modules. The chassis was also common across the computers. These modules use state of the art processors. They are designed as independent modules to do a specific function such as generating computer generated imagery for display on HUD or MFD. But they are able to communicate with the main processor module through high speed Dual Ported RAMs. This makes development of software for these specific functions as independent activities. Also, hardware changes in one module do not affect the other modules. Hence this approach utilizes the benefits of an Open System Architecture.T he CAC is housed in an aircraft industry standard 3/4 th ATR chassis with an option rear mount ARINC 404 connector or front mounted 38999 series connectors. The tray is mounted in the equipment bay/rack of the aircraft and the computer is plugged in to the tray. It is forced air cooled and weighs less than 8 kg. At present however, the MKI uses two Mission Computers and two Display Processors. These four units could possibly be replaced by two CAC's or two of the new DARE CPCi based open architecture computers. The DARE is also working on a more powerful CPCi based open architecture computer as well as developing a Power PC 7400 based open architecture computer around the VME standard, for the Light Combat Aircraft. This also combines mission processing, display processing and a video switching unit in a compact line replaceable unit.

HAL and DARE are currently working with SAMTEL India, a prominent Indian manufacturer of television displays, for the development of new multifunctional displays (MFD) which are to be superior to the original Sextant Avionique units currently used on the MKI. These displays will be able to simultaneously display both analogue and digital data on the same screen, and hence help in improved situational awareness for the aircrew.

DARE has developed and inducted the High Accuracy Direction Finding (HADF) payload, on a Siva pod, for the MKI. As the name suggests, this is a direction finding sensor, which works in combination with the onboard Tarang RWR.

[edit] Further improvements to the MKI

Other improvements suggested include a higher proportion of composites in the airframe, drawn from the Indian experience with the Light Combat Aircraft, whose airframe is 90% composite by surface area, and 45% by weight. Such a move, would assist in:

Weight reduction hence improving the aircraft performance
Reduce its radar cross section.

[edit] Powerplant

The Su-30MKI is powered by the two Al-31FP turbofans (P for povorotnoye meaning "movable"), which is a development of the Al-37FU (seen in the Su-37). Each Al-31FP is rated at 12,500 kgf (27,550 lbf) of full afterburning thrust

Al-31FP builds on the Al-37FU with the capability to vector in 2 planes. The TVC nozzles of the MKI deflect 32 degrees in the horizontal plane and 15 degrees in the vertical plane. This is done by angling them inwards by 15 degrees inwards, which produces a cork-screw effect and thus enhancing the turning capability of the aircraft.
The TVC nozzles will be made of titanium to reduce the nozzle's weight. The two nozzles can be vectored unsymmetrically, i.e. each nozzle can point at different directions independent from the other nozzle and thus multiplying the effect.
Two AL-31FP by-pass thrust-vectoring turbojet reheated engines (25,000 kgf full afterburning thrust) ensure a 2M horizontal flight speed (a 1350 km/h ground-level speed) and a rate of climb of 230 m/s. The mean time between overhaul for the AL-31FP is given at 1,000 hours with a full-life span of 3,000 hours. The titanium nozzle has a mean time between overhaul of 500 hours.

There is no a strain-gauge engine control stick to change the engine thrust in the cockpit, rather just a conventional engine throttle control lever. The pilot controls the aircraft with help of a standard control stick. On the pilot's right there is a switch which is turned on for performing difficult maneuvers. After the switch-over, the computer determines the level of use of aerodynamic surfaces and swiveling nozzles and their required deflection angles.

[edit] Range and fuel system

The Su-30MKI has a range of 3,000 km with internal fuel which ensures a 4.5 hour combat mission.
Also, it has an in-flight refueling (IFR) probe that retracts beside the cockpit during normal operation. The air refuelling system increases the flight duration up to 10 hours with a range of 8,000 km at a cruise height of 11 to 13 km.
The IAF in cooperation with the Defence Food Research Laboratories (DFRL) has designed inflight meals to provide nutrition to pilots flying long duration missions.
Su 30 MKIs also can use the Mk 32B buddy-buddy refueling pods.

[edit] Health and usage monitoring system

Russian Aircraft are often criticized on account of poor serviceability. For acquiring predictive maintenance capability, the IAF joined forces with South Africa's Aerospace Monitoring And Systems Ltd which developed a health and usage monitoring sysem.

Predictive maintenance refers to the on and off board processing of aircraft sub-systems data, resulting in an accurate, conclusive indication of the health and usage status of various airborne systems
The Su-30MKI on-board health and usage monitoring system (HUMS) monitors almost every aircraft system and sub-system including the avionics sub-systems. It can also act as an engineering data recorder

The Indian Air Force's Software Development Institute has also developed its own Health and Usage Monitoring systems as well as Mission Planning Systems, which are stated to be comparable to other products available internationally. Variants of these may also be used on Indian made MKIs.

The Su-30 MKI's avionics also feature modular components as well as extensive reliance on BITE or Built In Tests, so as to assist maintenance personnel with quickly locating and rectifying/ replacing defective avionics items.

[edit] Weapons and payload

The Su-30MKI combat load is mounted on 12 stations. The maximum advertised combat load is 8000 kg (17,600 lb). The aircraft features the built-in single-barrel GSh-301 gun, a 30 mm weapon, and space for 150 rounds. Over 70 versions of guided and unguided weapon stores may be employed, which allows the aircraft to fly the most diverse tactical missions.

Armament: The ranges mentioned should be taken as indicative, since they vary based on flight profile, target characteristics, flight profile as well as several other factors.

Air to Air Missiles:

6 X R-27R/AA-10A semi-active radar homing medium range AAM of range 80 km.
6 X R-27T(AA-10B) infrared homing seeker, medium range AAM, 70 km
2 X R-27P(AA-10C) passive radar seeker, long range AAM
10 X R-77(AA-12) active radar homing medium range AAM, 100 km
6 X R-73(AA-11) short range AAM, 30 km

Air to Surface Missiles:

2 X Kh-59ME TV guided standoff Missile, 115 km
4 X Kh-31P/A anti-radar missile, 70 km
6 X Kh-29T/L laser guided missile, 30 km
4 X S-8 rocket pods (80 unguided rockets)
4 X S-13 rocket pods (20 unguided rockets)

Bombs:

6 X KAB-500L laser guided bombs
3 X KAB-1500L laser guided bombs
8 X FAB-500T dumb bombs
28 X OFAB-250-270 dumb bombs
8 X RBK-500 cluster bombs

Pods:

APK-9 (Datalink Pod for the KH-59 Missile)
Cobham Flight Refuelling pod, 754 series ^[4]
IAI - Elta EL/L-8222 (RF jammer)
Rafael LITENING Laser Targeting Pod.
DARE (DRDO) High Accuracy Direction Finding (HADF) pod

[edit] Specifications (Sukhoi Su-30MKI)

General characteristics

Crew: Two
Length: 22.10 m (72 ft 51 in)
Wingspan: 14.70 m (48 ft 23 in)
Height: 6.38 m (22 ft 89 in)
Wing area: 62.04 m² (667.8 ft²)
Empty weight: 24,900 kg (54,900 lb)
Loaded weight: 34,500 kg (76,100 lb)
Max takeoff weight: 38,800 kg (85,554 lb)
Powerplant: 2× Lyulka AL-31FP turbofans with thrust vectoring, 131 kN (29,400 lbf) each

Performance

Maximum speed: Mach 1.10, 1,350 km/h at sea level; Mach 2+, 2,135+ km/h at 11,000 m (840 mph at sea level / 1,330+ mph at 36,000 ft)
Range: 3,000 km (1864 mi)
Service ceiling: 18,000 m (59,000 ft)
Rate of climb: 230 m/s (45000 ft/min)
Wing loading: 556 kg/m² (113 lb/ft²)
Thrust/weight: 0.77

[edit] References

^ [1].
^ [2].
^ [3].
^ [4].

[edit] External links

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