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 (izdeliye "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.

The MiG-29Ks first flight was performed on 23 July 1988 at Saky by test pilot Toktar Aubakirov.
On 1 November 1989, on the same day as the Sukhoi Su-27K, Aubakirov executed the first carrier landing of MiG-29K on the aircraft-carrying cruiser Tbilisi (now known as Admiral Kuznetsov), the first take-off from the carrier's deck was successfully performed the same day.
During 1989–1991, the MiG-29K underwent further tests aboard Admiral Kuznetsov.
The project was put on hold with the collapse of the Soviet Union, while the Russian Navy only pursued the rival Su-33.
Mikoyan continued work on the MiG-29K despite the lack of funding.

During its tests aboard Admiral Kuznetsov, the aircraft had a springboard-assisted takeoff from strips 195 metres (640 ft) and 95 m (312 ft) long.
According to the results of the tests, the landing accuracy proved to be very high, which made it possible at a later stage to switch over to a three-cable arrester system on Admiral Gorshkov.
The landing accuracy is additionally enhanced through the employment of an autothrottle system.
The takeoff characteristics allow for most flights to be possible under tropical conditions at a ship speed of 10 knots (19 km/h; 12 mph).
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 (izdeliye "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.
The MiG-29Ks first flight was performed on 23 July 1988 at Saky by test pilot Toktar Aubakirov. On 1 November 1989, on the same day as the Sukhoi Su-27K, Aubakirov executed the first carrier landing of MiG-29K on the aircraft-carrying cruiser Tbilisi (now known as Admiral Kuznetsov), the first take-off from the carrier's deck was successfully performed the same day. During 1989–1991, the MiG-29K underwent further tests aboard Admiral Kuznetsov. The project was put on hold with the collapse of the Soviet Union, while the Russian Navy only pursued the rival Su-33. Mikoyan continued work on the MiG-29K despite the lack of funding.
During its tests aboard Admiral Kuznetsov, the aircraft had a springboard-assisted takeoff from strips 195 metres (640 ft) and 95 m (312 ft) long. According to the results of the tests, the landing accuracy proved to be very high, which made it possible at a later stage to switch over to a three-cable arrester system on Admiral Gorshkov. The landing accuracy is additionally enhanced through the employment of an autothrottle system. The takeoff characteristics allow for most flights to be possible under tropical conditions at a ship speed of 10 knots (19 km/h; 12 mph).
Mikoyan MiG-29K