Background and origins During the 1970s, the
Yakovlev Yak-38, then the
Soviet Navy's only operational carrier-based fixed-wing combat aircraft, was found to be unable to undertake its role due to limited range and payload, which severely hampered the capability of the Soviet Navy's
Project 1143 carriers. It was decided to develop a bigger and more potent carrier capable of operating STOL aircraft. During the assessment period, a number of aircraft carriers were studied; the Project 1160 carrier would have been able to operate the
MiG-23s and
Su-24s, but was abandoned due to budget constraints. Design efforts were then concentrated on the
Project 1153 carrier, which would have accommodated the
Su-25s and the proposed MiG-23Ks and Su-27Ks. Sufficient funding was not secured, and the Navy looked at the possibility of a fifth, and larger, Project 1143 carrier, modified to allow for
Yak-141,
MiG-29K and Su-27K operations. To prepare for the operations of the Su-27K and the rival MiG-29K on board the new carrier, work proceeded on the development of the
steam catapult,
arresting gear, optical and radio landing systems. The pilots were trained at a new establishment in
Crimea, named NITKA, for Aviation Research and Training Complex. In 1981, the Soviet government ordered the abandonment of the catapult system as part of an overall downsize of
Project 1143.5 carriers, which also included cancelling the fifth Project 1143 carrier and
Varyag. A takeoff ramp was installed at the complex, where takeoffs would be executed to ensure that the Su-27Ks and MiG-29Ks would be able to operate from carriers. Both Sukhoi and Mikoyan modified their prototypes to validate the takeoff ramp. Three Sukhoi T10s (−3, −24 and −25), along with an Su-27UB, were used for takeoffs from the simulated ramp. The first of these tests were undertaken by Nikolai Sadovnikov on 28 August 1982. Flight tests indicated the need for a change in ramp design, and it was modified to a
ski-jump profile. Full-scale design of the Su-27K soon started as the "T-10K" under the guidance of Konstantin Marbyshev. Nikolai Sadovnikov was appointed the
design bureau's Chief Test Pilot for the programme. By November 1984, conceptual design had passed its critical design review, with the detailed design finalised in 1986. The two prototypes were constructed in conjunction with KnAAPO in 1986–1987. It was found that the carrier's
jet blast deflectors were too close to the engine nozzles when raised at an angle of 60°; thus an improvised solution held the deflectors at 45°. However, when the aircraft was in front of it for longer than the maximum six seconds, the shield's water pipes exploded. The pilot, Pugachyov, reduced engine throttle, accidentally causing the detents (blocks used to restrain aircraft from accelerating) to retract and the fighter to move forwards. The aircraft was quickly stopped; Pugachyov later took off without the use of blast deflectors or detents. Since then, a
Kamov Ka-27PS search-and-rescue helicopter was flown close to the carrier in case of an accident. During the following three-week period, 227 sorties were amassed, along with 35 deck landings. Notable improvements over the Su-33 included a revised forward fuselage and leading edge slats, bigger wings and
stabilators.
Modernization In 2010, Sukhoi developed an upgraded version of the Su-33; flight trials began in October 2010. This modernized Su-33 was to compete with a potential Chinese indigenous version of the original Su-33, the
Shenyang J-15, and to encourage orders from the Russian Navy. Major upgrades to the aircraft included more powerful (132 kN, 29,800 lbf) AL-31-F-M1 engines and a larger weapons carriage; upgrades to the radar and weapons were not possible at the time due to funding constraints. According to military author Richard Fisher, it has been speculated that further modifications to a new production batch would include a phased-array radar, thrust vectoring nozzles, and long-range anti-ship missiles. It is believed, the installation of modern targeting systems will increase the capability of the Su-33 fighters close to
Su-30SM level. The second stage of the modernization is to include installation of more powerful engines and detection systems, according to Naval Aviation Chief Major-General Igor Kozhin. == Design ==