MiG-29 SM
The MiG-29SM is a multi-role fighter with improved airborne avionics and enhanced nomenclature of high precision weapons capable to destroy the air and ground (surface) targets. At development of the MiG-29SM aircraft version the main attention was paid to reduction of the up-grading cost and terms.
The MiG-29 aircraft upgrading to the MiG-29SM version results in inclusion into the N-019E (N-019ME) airborne radar composition of an independent radar-channel with MVK-04 computer, in upgrading of the optical electronic fire control & navigation system due to integration of a new data display system with a MFD-54 multifunction color display and installation of additional weapons management control system. The flight-navigation and radio-communication equipment is added with the multifunctional computer, GPS receiver and additional radio-station. It is provided for the use of a new electronic counter-measures system in pod.
In the composition of MiG-29SM airborne avionics the data exchange multiplex channel is added (bus of MIL STD 1553B standard).
The "A-A" class weapons nomenclature is added with middle-range missiles R-27ER1, R-27ET1 (T1) with radar-guided and IR homing heads and RVV-AE missiles with active radar homing heads.
The up-graded weapons management system ensures the application of high precision weapons of the "A-S" class: Kh-29T (TE), Kh-31A, Kh-31P missiles and guided bombs KAB-500Kr and KAB-500-OD. While using the target designation pod or target external illumination it is possible to apply the Kh-29L, Kh-25ML missiles as well as the laser guided bombs.
It is possible to adapt the MiG-29SM aircraft to the NATO and/or ICAO standards.
While upgrading the original aircraft to the MiG-29SM version the following optional works can be fulfilled:
– aircraft structure reinforcement for the extension of flight hours and service life up to 100% (depending on the aircraft technical condition);
– increase of internal fuel tanks capacity;
– installation of in-flight refueling systems of different types;
– improvement and/or replacement of some airborne systems;
– repair and transfer to on-condition maintenance.
– aircraft structure reinforcement for the extension of flight hours and service life up to 100% (depending on the aircraft technical condition);
– increase of internal fuel tanks capacity;
– installation of in-flight refueling systems of different types;
– improvement and/or replacement of some airborne systems;
– repair and transfer to on-condition maintenance.
The MiG-29 aircraft upgrading to the MiG-29SM version can be fulfilled without aircraft delivery to Russia. The Customer’s companies or of the third countries may be involved into upgrading.
The equipment required for MiG-29 aircraft upgrading to the MiG-29SM version as well as appropriate algorithmic description and software have been already tested aboard the aircraft and is in serial production and operation with Customer.
Besides the upgrading of the previously supplied aircraft, the new aircraft of the MiG-29SM type can be manufactured.
MiG-29 SMT
The MiG-29SMT aircraft is a fundamental upgrading of the original MiG-29 aircraft which is the multi-role fighter of "4+" generation with avionics open architecture and continuously enhanced nomenclature of high precision weapons.
The MiG-29SMT aircraft is in serial production since 2004 and is supplied to customers. The RAC "MiG" also upgrades the aircraft previously supplied to a number of Customers into the MiG-29SMT type.
The MiG-29SMT main features:
– Modern high precision weapons of "A-S" class are included into the weapons nomenclature. It is provided for the weapons nomenclature enhancement during aircraft life cycle.
– The aircraft is equipped with multifunctional multi-mode pulse-Doppler airborne "Zhuk-ME" radar manufactured by "Fazotron-NIIP" Corporation. The radar is provided with a slot antenna array. As compared with the airborne radar of the previous generation the "Zhuk-ME" has enhanced scanning angles in azimuth, twice increased detection range, less weight and higher reliability. The "Zhuk-ME" radar provides for tracking up to 10 air targets with capability of simultaneous firing of 4 targets with missiles.
– The airborne avionics of the MiG-29SMT aircraft is designed following the principle of open architecture on the basis of a mission computer with the data exchange multiplex channel (bus of MIL STD 1553B standard). It allows to install aboard the aircraft the new systems of Russian or foreign origin at the customer’s request.
– The cockpit data display system includes two new wide-screen MFD-10-6 multifunction color displays and realizes the HOTAS conception.
– INS-GPS navigation system is included into the navigation equipment.
– The aircraft is equipped with in-flight refuelling system.
– Modern high precision weapons of "A-S" class are included into the weapons nomenclature. It is provided for the weapons nomenclature enhancement during aircraft life cycle.
– The aircraft is equipped with multifunctional multi-mode pulse-Doppler airborne "Zhuk-ME" radar manufactured by "Fazotron-NIIP" Corporation. The radar is provided with a slot antenna array. As compared with the airborne radar of the previous generation the "Zhuk-ME" has enhanced scanning angles in azimuth, twice increased detection range, less weight and higher reliability. The "Zhuk-ME" radar provides for tracking up to 10 air targets with capability of simultaneous firing of 4 targets with missiles.
– The airborne avionics of the MiG-29SMT aircraft is designed following the principle of open architecture on the basis of a mission computer with the data exchange multiplex channel (bus of MIL STD 1553B standard). It allows to install aboard the aircraft the new systems of Russian or foreign origin at the customer’s request.
– The cockpit data display system includes two new wide-screen MFD-10-6 multifunction color displays and realizes the HOTAS conception.
– INS-GPS navigation system is included into the navigation equipment.
– The aircraft is equipped with in-flight refuelling system.
Aircraft can be equipped with ECM system installed in pod. At the customer’s request the MiG-29SMT aircraft can be equipped with the upgraded IRSTS system as well as with radio-stations, navigation equipment and IFF transponders of different types.
According to avionics architecture and weapons nomenclature the MiG-29SMT aircraft is unified with a new generation of the RAC "MiG" fighters family.
The double-seat version of the MiG-29SMT aircraft is called the upgraded MiG-29UB. It has the same avionics structure and identical cockpit data display system composition but it has no radar. The upgraded MiG-29UB aircraft has the same weapons as the MiG-20SMT except for weapons with radar homing heads (for training purposes the simulation mode is provided).
For both the MiG-29SMT and upgraded MiG-29UB aircraft the complete set of training means has been developed.
While upgrading the previously supplied aircraft to the MiG-29SMT version the following optional works can be fulfilled:
– aircraft structure reinforcement for the extension of flight hours and service life (depending on the aircraft technical condition);
– increase of internal fuel tanks capacity;
– installation of in-flight refueling systems of different types;
– improvement and/or replacement of some airborne systems;
– repair and transfer to on-condition maintenance.
– aircraft structure reinforcement for the extension of flight hours and service life (depending on the aircraft technical condition);
– increase of internal fuel tanks capacity;
– installation of in-flight refueling systems of different types;
– improvement and/or replacement of some airborne systems;
– repair and transfer to on-condition maintenance.
Su-30 SME
President of Irkut Corporation Oleg Demchenko revealed performance specifications for the twin-seat derivative of the Su-30SM that recently entered service with Russia and Kazakhstan (the Su-30SM is itself a development of the Su-30MKI sold to India).
The Su-30SME has a normal take-off weight of 26,090 kg, a maximum take-off weight of 34,000 kg, a speed of 1.75 Mach, and normal/maximum fuel weights of 5,270/9,300 kg respectively. It has operational range of 1,280 km at sea-level and at a speed of 800 km/h; of 3,000 km flying at a high altitude and at a speed of 900 km/h; and of 5,600 km with one air refuelling contact.
The Su-30SME is powered by two AL-31FP afterburner jet engines with thrust vectoring control. The powerplants have a combined thrust of 25,000 kg, and afford the fighter a combat payload of up to 8,000 kg mounted from its 12 hardpoints.
The avionics suite of the Su-30SME has been upgraded and the aircraft equipped for infrared and laser targeting pods for ground target acquisition and engagement. The new fire control radar can acquire and track 15 aerial targets simultaneously while being able to attack four at once. Other features include an integrated electro-optical targeting sensor coupled with a laser inertial navigation system, a helmet-mounted target designator, and satellite navigation system compatible with the GLONASS and NAVSTAR formats.
"The Su-30SME is an upgraded modern platform based on Russian equipment," Demchenko said. "As the basic Russian Su-30SM version develops, the capabilities of the export Su-30SME will also expand."
Su-30 SM
Su-30SM is a multirole fighter aircraft developed by JSC Sukhoi Design Bureau for the Russian Air Force. It is an advanced derivative of the Su-30MK combat aircraft family.
The Su-30SM fighter was designed in accordance with the requirements of the Russian Air Force. It is being manufactured by IRKUT, a company based in Russia. The first Su-30SM fighter designed for the Russian Ministry of Defence (MoD) performed its maiden flight in September 2012.
The multirole Su-30SM can be deployed in counter-air strikes, counter-land and counter-sea missions. It can conduct electronic counter-countermeasures and early warning tasks. The aircraft also acts as a command-and-control platform within a fleet of combat aircraft performing joint missions.
The airframe of Su-30SM is made of titanium and high-strength aluminium alloys. It is based on the Su-30MKI aircraft developed jointly by IRKUT and JSC Sukhoi Design Bureau, for the IAF (Indian Air Force).
The fuselage head houses cockpit, radar sections and avionics bay. High manoeuvrability was achieved through the integral aerodynamic form combined with a thrust vectoring feature.
The glass cockpit accommodates two pilots in tandem configuration. The crew are provided with ejection seats. The cockpit incorporates an advanced avionics suit integrating a head-up display and liquid crystal multifunction displays.
The Su-30SM features identification friend-or-foe equipment, a global positioning system and an inertial navigation system. The open architecture design allows the integration of modern avionics, including a new radar system, radio and recognition system, and other support systems.
The Su-30SM is capable of carrying an advanced weapons payload weighing up to 8t. The aircraft can be armed with a machine gun, bombs, air-to-air missiles, and Oniks (Yakhont) supersonic anti-ship and land attack missiles. Developed by NPO Mashinostroyeniya, Oniks served as a basis for the BrahMos supersonic missile. Oniks has an operational range of 120km to 300km depending on altitude.
The aircraft can engage aerial threats, ground and naval surface targets by deploying onboard air-to-air and air-to-surface guided/unguided weapons. It can be fitted with anti-surface weaponry such as rockets and rocket pods for conducting land attack operations.
The Su-30SM is powered by two AL-31FP by-pass turbojet reheated engines. The engines generate a total after-burning thrust of 25,000kgf. The power plant provides a horizontal flight speed of Mach 2.
The maximum unrefuelled flight range of Su-30SM is 3,000km. The aircraft is also equipped with a flight refuelling probe and system.
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