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Sukhoi Su-33 ASCC codename: Flanker Carrier-borne Multi-Role Fighter |
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DESCRIPTION:
The Sukhoi Su-33 is a navalized version of the company's Su-27 originally designed to operate from the Soviet Union's first class of large aircraft carriers. To meet the requirements of shipboard duty, the Su-33 features a strengthened airframe, corrosion resistance, arrestor gear, more powerful engines, and wing and tailplane folding mechanisms for storage aboard ship. The Su-33 is also the first member of the Su-27 family fitted with canards near the juncture of the wing and leading edge extension allowing better maneuverability while reducing the takeoff distance and landing speed. The Su-27K, as the design was first known, was originally developed for the Soviet Navy alongside the MiG-29K. It was envisioned that both aircraft would be purchased for carrier operations. However, the collapse of the Soviet Union left the Russian Navy with only one Kuznetsov class carrier, and the decision was made to acquire just one aircraft type for carrier use. Although more expensive and larger, meaning fewer could be carried, the Navy chose the Su-27K over the competing MiG-29K. About 24 aircraft, now designated as the Su-33 by Sukhoi, were purchased. Unfortunately, budget cuts have forced the elimination of the aircraft carrier and these aircraft now operate from shore bases. A further development of the basic airframe is the two-seat Su-27KUB (or Su-33UB) trainer that features the side-by-side seating arrangement of the Su-34 family.
Last modified 13 October 2007
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| HISTORY: | |
| First Flight |
(Su-27K) May 1985 (Su-27KUB) 29 April 1999 |
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Service Entry
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1994
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| CREW: |
one: pilot
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ESTIMATED COST:
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unknown
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| AIRFOIL SECTIONS: | |
| Wing Root | unknown |
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Wing Tip
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unknown
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| DIMENSIONS: | |
| Length | 71.92 ft (21.94 m) |
| Wingspan | 48.17 ft (14.70 m) |
| Height | 19.42 ft (5.92 m) |
| Wing Area | 666 ft2 (62.0 m2) |
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Canard Area
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unknown
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| WEIGHTS: | |
| Empty | 35,275 lb (16,000 kg) |
| Normal Takeoff | 49,605 lb (22,500 kg) |
| Max Takeoff | 70,545 lb (32,000 kg) |
| Fuel Capacity |
internal: 20,725 lb (9,400 kg) external: unknown |
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Max Payload
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14,330 lb (6,500 kg)
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| PROPULSION: | |
| Powerplant | two Saturn/ Lyul'ka AL-31F afterburning turbofans |
| Thrust |
61,730 lb (274.6 kN)
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| PERFORMANCE: | |
| Max Level Speed |
at altitude: 1,430 mph (2,300 km/h) at 32,780 ft (10,000 m), Mach 2.17 at sea level: 870 mph (1,400 km/h), Mach 1.1 cruise speed: 870 mph (1,400 km/h) at 32,780 ft (10,000 m) |
| Initial Climb Rate | 45,235 ft (13,800 m) / min |
| Service Ceiling | 55,720 ft (17,000 m) |
| Range |
typical: 1,620 nm (3,000 km) ferry: unknown |
| g-Limits |
+9
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| ARMAMENT: | |
| Gun | one 30-mm GSh-301 cannon (149 rds) |
| Stations | ten external hardpoints and two wingtip rails |
| Air-to-Air Missile | R-27/AA-10 Alamo, R-73/AA-11 Archer, R-77/AA-12 |
| Air-to-Surface Missile | Kh-25MP/AS-12 Kegler, Kh-31/AS-17 Krypton, Kh-41 |
| Bomb | various |
| Other |
rocket pods, ECM pods
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| KNOWN VARIANTS: | |
| T-10K | Prototype of the Su-27K |
| Su-27K 'Flanker-D' | Official designation of the Su-33 used by the Russian Navy |
| Su-33 'Flanker-D' | Production model with canards, strenthened structure, folding wings and tailplanes, arrester hook, uprated engine, corrosion protection, an in-flight refueling probe, and other modifications to make the aircraft suitable for carrier operations; approximately 24 built |
| Su-33UB or Su-27KUB |
Side-by-side two-seat combat-capable trainer similar to the
Su-32 or Su-34 but retaining the more rounded nose of the Su-33
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| KNOWN COMBAT RECORD: |
none
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| KNOWN OPERATORS: |
Russia, Aviatsiya Voyenno-Morskoyo Flota (Russian Naval Aviation)
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3-VIEW SCHEMATIC:
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SOURCES:
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