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Su-33 Sukhoi
Su-33
ASCC codename: Flanker
Carrier-borne Multi-Role Fighter

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

HISTORY:
First Flight (Su-27K) May 1985
(Su-27KUB) 29 April 1999
Service Entry

1994

CREW: one: pilot

ESTIMATED COST:

unknown

AIRFOIL SECTIONS:
Wing Root unknown
Wing Tip

unknown

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)
Canard Area

unknown

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
Max Payload

14,330 lb (6,500 kg)

PROPULSION:
Powerplant two Saturn/ Lyul'ka AL-31F afterburning turbofans
Thrust 61,730 lb (274.6 kN)

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

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

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

KNOWN COMBAT RECORD: none

KNOWN OPERATORS: Russia, Aviatsiya Voyenno-Morskoyo Flota (Russian Naval Aviation)

3-VIEW SCHEMATIC:

Su-33


SOURCES:





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