MiG-29K
| MiG-29K | |
|---|---|
 |
|
| MiG-29K of the Indian Navy | |
| Role | Carrier-based multirole fighter |
| National origin |
Soviet Union Russia |
| Manufacturer | Mikoyan |
| First flight | 23 July 1988 |
| Introduction | 19 February 2010 |
| Status | In production |
| Primary users |
Indian Navy Russian Navy |
| Produced | 2005–present |
| Unit cost |
$32 million
|
| Developed from | Mikoyan MiG-29M |
| MiG-29 overview | |
 Poster by RIA Novosti
|
The Mikoyan MiG-29K (Russian: Микоян МиГ-29K, NATO reporting name: Fulcrum-D) is a Russian all-weather carrier-based multirole fighter aircraft developed by the Mikoyan design bureau. The MiG-29K was developed in the late 1980s from MiG-29M. Mikoyan describes it as a 4++ generation aircraft.
Production MiG-29Ks differ from prototypes by features such as a multi-function radar and several new cockpit displays; the adoption of HOTAS (hands-on-throttle-and-stick) controls; the integration of RVV-AE (also known as R-77) air-to-air missiles, along with missiles for anti-ship and anti-radar operations; and several ground/strike precision-guided weapons.
The MiG-29K was not ordered into production and only two prototypes were originally built because the Russian Navy preferred the Su-27K (later re-designated Su-33) in the early 1990s. The Mikoyan Design Bureau did not stop its work on the MiG-29K aircraft despite the lack of financing since 1992. The programme got a boost in the late 1990s to meet an Indian requirement for a ship-borne fighter following the purchase of a former Soviet aircraft carrier, and the MiG-29K was first received by the Indian Naval Air Arm in 2009. The Russian Navy, with their Su-33s nearing the end of their service lives by 2010, has also ordered the MiG-29K as a replacement.
The MiG-29K project was initiated in the late 1970s when the Soviet Navy developed a requirement for a supersonic carrier-based fighter. As a first step to meet this requirement, the Mikoyan design bureau designed a "proof of concept" version of the MiG-29 fitted with a stronger undercarriage and a reinforced tail section with an arrestor hook, the MiG-29KVP (Korotkii Vzlet i Posadka, or "short take off and landing"). The KVP first flew on 21 August 1982, and was subject to extensive trials which demonstrated it could safely operate from a ski-jump, but ideally a production aircraft needed more power and greater wing area. It was decided to base the definitive naval version on the advanced MiG-29M (Product 9.15) that was already under development, further modified with new undercarriage and folding wings of greater area, with the new model designated the MiG-29K (Korabelniy – "ship based") or Project 9–31. The MiG-29K differed considerably from the MiG-29 production model, featuring a new multi-function radar, dubbed Zhuk; a cockpit with monochrome display and use of the HOTAS (hands-on-throttle-and-stick) principle; the RVV-AE air-to-air active homing missiles; antiship and antiradar missiles; as well as air-to-ground precision-guided weapons. To protect the engine from foreign object damage (FOD), the engine inlets were fitted with retractable grills for air flow, rather than metal doors and leading-edge extension auxiliary intake louvres used by land-based MiG-29s.
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