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MiG-29M
MiG-29M
Role Fighter
National origin Russia
Manufacturer Mikoyan
Primary user Russian Air Force
Developed from Mikoyan MiG-29
Variants Mikoyan MiG-29K

The Mikoyan MiG-29M (Russian: Микоян МиГ-35, NATO reporting name "Fulcrum-E") is a mature development of the MiG-29M/M2 and MiG-29K/KUB technology. Formerly known as the "MiG-33", it was developed from the Mikoyan MiG-29 (NATO: "Fulcrum") fighter jet during mid-1980s. The MiG-29M is sometimes called the Super Fulcrum.

Contents

[edit] Development

In the mid-1980s, a development of the original MiG-29 was proposed to meet the Soviet western front line requirement. It was required to be a multi-role fighter for the front line defensive air force to gain offensive strike ability.[1] This development resulted in a single seat and a double seat variant. The proposal was then grounded as a result of shift in military strategy. The model was named "MiG-33" and later received the MiG-29ME designation for export market in the mid-1990s. A twin seat model of the standard, commonly known as the MiG-29MRCA, was the MAPO-MiG's primary contender for many international fighter aircraft bids, later evolved into the Mikoyan MiG-35. Six of these models were built before 1990.[2] They were constantly upgraded with various components and one received experimental vector thrust engines which eventually became the MiG-29OVT. The model was again renamed as MiG-29M.[3] The MiG-29M/M2 now belongs to the "New unified family" instead of the "MiG-29 fighters family" which comprise the older variants.

RAC MiG engineers have continually upgraded the model for better performance, seeking a possible sale of the aircraft. The innovations focused on aerodynamics improvements, fly-by-wire technology, stealth features, increased fuel capacity and in-flight refueling solutions, more weight load, and well established open architecture for application of foreign equipment. Together with the success of MiG-29K/KUB and MiG-35, the MiG-29M/M2 also took advantage of new technologies, such as the new enhanced thrust smokeless engines. New reliability measures resulted in a decrease of flight hour cost by about 2.5 times and the capability of on-condition maintenance. These new technologies gave the aircraft contemporary features to fourth and fifth generation fighters, and most important, gave the aircraft a true multi-role capability.

Furthermore, the RAC MiG engineers have also developed a set of training simulators to help pilots master the sophisticated controls of the new aircraft. The simulators' interactive computer-based training systems offer full-mission motion simulations.

[edit] Design

Facts based on [3][4]

[edit] Features

The MiG-29M/M2 aircraft is a revision of the basic MiG-29. It achieved a more robust multi-role capability with enhanced use of air-to-air and air-to-ground high-precision weapons. It also featured considerably increased combat range owing to an increase in its internal fuel capacity. Along with a better pilot-to-aircraft interface in the cockpit, a digital three-channel fourfold redundant fly-by-wire system, improved navigation, radio communications, electronic countermeasures, monitoring and recording systems, and optronic and reconnaissance pods, have improved overall aircraft performance considerably.

[edit] Airframe evolutions

A few changes took place during the development of the MiG-33. The redesigned airframe was constructed from a lightweight aluminum-lithium alloy to increase thrust-to-weight ratio. Air intakes' geometry was revised, the upper intake louvers removed to make way for more fuel in the LERXs, mesh screens introduced to prevent foreign object damage (FOD) and enlarged inlet dimensions for higher airflow. The back of the aircraft featured an enlarged spine for more fuel capacity and a dorsal air break. Radome and canopy were redesigned to give space for avionic upgrades. Aerodynamics were also revised. The wings increased span and aileron, while the tail fins revised trailing edges.

[edit] Powerplant

The RD-33MK, the latest revision of the RD-33, has 7% more power in comparison to the baseline model due to the usage of modern materials on the cooled blades, it provide a thrust of 9,000 kgf. In response to long time criticism, the new engines are smokeless and contain improvements that reduce its infrared visibility. Thrust vectoring nozzles are now offered upon customer’s request.[5][6]

[edit] Range and fuel system

The aircraft is built with an in-flight-refueling (IFR) probe and is able to carry three fuel drop tanks. The redesigned airframe also significantly increased internal fuel capacity in the dorsal spine and LERXs fuel tanks. These give the aircraft of single seat an operation range of 2,000 km with internal fuel, 3,200 km with three fuel drop tanks, and 6,000 km with three drop tanks and in-flight-refueling.

[edit] Cockpit

The cockpit has been redesigned to incorporate contemporary features. While some analogue instruments have been retained, two monochrome liquid crystal (LCD) multi-function displays (MFD) have been introduced and new weapon controls have been incorporated in a HOTAS concept. Other new features include the Zhuk-ME radar, an infra-red search and track (IRST) system and a helmet-mounted target designation system (early HMD).

[edit] Sensors

Main upgrades consists the Zhuk-ME pulse-Doppler airbone radar, along with revised IRST systems, helmet-mounted target designation system and electronic countermeasures. New radar capable of detecting air targets at ranges up to 120 km, track-while-scan of ten targets and attack of four targets at a time. In scanning surface targets, the radar detection range of destroyer-type targets is 250 km and that of missile launcher-type targets is 150 km. Hence beyond visual range (BVR) engage is greatly enhanced.

[edit] Armament

The aircraft can carry the RVV-AE (R-77), R-27ER1, R-27ET1, R-27R1, R-27T1, R-73E air-to-air missiles, the Kh-29T, Kh-29L, Kh-31A, Kh-31P, Kh-35E air-to-surface missiles, the KAB-500KR (OD), KAB-500L guided bombs, as well as rockets and free-fall bombs. The aircraft retains the GSh-301 built-in gun.

[edit] Operators

 Russia
Future operators
 Syria

[edit] Specifications (MiG-29M/M2)

Data from MiG-29M data,[8] Warfare.ru,[9] Global Security[10]

General characteristics

  • Crew: 1 or 2
  • Length: 17.37 m (57 ft)
  • Wingspan: 11.4 m (37 ft 3 in)
  • Height: 4.73 m (15 ft 6 in)
  • Wing area: 38 m² (409 ft²)
  • Max takeoff weight: 22,400 kg (49,383.54 lb)
  • Powerplant:Klimov RD-33MK afterburning turbofans, 9,000 kgf (88.26 kN, 19,840 lbf) each

Performance

Armament

Avionics

[edit] See also

Related development

Comparable aircraft

Related lists

[edit] References

  1. ^ Lake, John, Jane's How to Fly and Fight in the Mikoyan MiG-29 (HarperCollins, 1997 ISBN 0-00472144-6), p.19.
  2. ^ Aviapedia » Mig-29VFT video from “Smotr” tv-series
  3. ^ a b Rac Mig
  4. ^ Lake, John. Jane's How to Fly and Fight in the Mikoyan MiG-29. (HarperCollins, 1997. ISBN 0-00472144-6)
  5. ^ Klimov :: Production :: Aircraft Program :: RD-33MK
  6. ^ MiG-29M/M2
  7. ^ "Damascus set to receive MiG 31E planes", Jerusalem Post, 29 March 2009.
  8. ^ MiG-29M2 product page
  9. ^ a b c d MIG-29/MIG-35 Fulcrum Counter-Air Fighter. Warfare.ru
  10. ^ MiG-33 page on GlobalSecurity.org
  • Gordon, Yefim and Peter Davison. Mikoyan Gurevich MiG-29 Fulcrum. Specialty Press, 2005. ISBN 978-1-58007-085-1.

[edit] External links




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