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Sukhoi Su-33 Naval Flanker

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Published on Mar 25, 2010

The Sukhoi Su-33 (NATO reporting name: Flanker-D) is a carrier-based multi-role fighter aircraft produced by Russian firm Sukhoi beginning in 1982. It is a derivative of the Su-27 Flanker and was initially known as the Su-27K. The main differences from the Su-27 are that the Su-33 can operate from aircraft carriers and is capable of aerial refueling.

Specifications (Su-33)
General characteristics
Crew: 1
Length: 21.94 m (72 ft)
Wingspan: 14.70 m (48.25 ft)
Height: 5.93 m (19.5 ft)
Wing area: 62.0 m² (667 ft²)
Empty weight: 18,400 kg (40,600 lb)
Loaded weight: 29,940 kg (66,010 lb)
Max takeoff weight: 33,000 kg (72,750 lb)
Powerplant: 2× AL-31F afterburning turbofans
Dry thrust: 7,600 kgf (74.5 kN, 16,750 lbf) each
Thrust with afterburner: 12,500 kgf (122.6 kN, 27,560 lbf) each
Wingspan, wings folded: 7.40 m (24.25 ft)
Performance
Maximum speed: Mach 2.17 (2,300 km/h, 1,430 mph) at 10,000 m (33,000 ft) altitude
Stall speed: 240 km/h (150 mp/h)
Range: 3,000 km (1,860 mi)
Service ceiling: 17,000 m (55,800 ft)
Rate of climb: 325 m/s (64,350 ft/min)
Wing loading: 483 kg/m²; (98.9 lb/ft²)
Thrust/weight: 0.83
Maximum turn: +8 g[12] (+78 m/s²)
Landing speed: 235-250 km/h (145-155 mph)
Armament
1 × 30 mm GSh-30-1 cannon with 150 rounds
Up to 6,500 kg (14,300 lb) of munitions on twelve external hardpoints, including:
R-27/R-73 air-to-air missiles
Various bombs and rockets
ECM pods

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