Photo Su-33KUB © Sukhoi Company (JSC)
Technical specifications 
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The Su-27KUB is a supersonic ship-borne twin-seater- a combat trainer being a derivative of the Su-33 (Su-27K) ship-borne single-seat fighter.
The aircraft features a side-by-side crew seating arrangement, expanded wing and empennage as well as a number of other improvements.
The first Su-27KUB prototype made its maiden flight on 29 April, 1999. The aircraft is in production at the KnAAPO.
TECHNICAL SPECIFICATIONS
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DESIGNER
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OKB Sukhoi
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COUNTRY
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Russia
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TYPE
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Shipborne fighter
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CREW
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2
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POWER-PLANT
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Two bypass engine, ΝPO Saturn Lyl'ka AL-31F Seria 3
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Thrust, kgf
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2 x 12.500
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DIMENSIONS
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Length, m
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22,00
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Height, m
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5,95
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Wing span, m
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14,90
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Wing area, m2
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64,5
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WEIGHT
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Empty aircraft, kg
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16.000
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Normal take-off, kg
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22.500
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Maximum take-off, kg
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30.000
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Internal fuel, kg
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9.400
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PERFORMANCE
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Maximum speed, km/h
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2.500
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Max speed in low height, km/h
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1.400
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Range, km
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3.900
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Service ceiling, m
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18.500
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Maximum overload, g
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9
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ARMAMENT
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1x30 mm cannon GSh-301(150 rounds)
Warload-6.000 kg in 12 hardpoints: Two Air-to-air missile R-27ER and R-27ET, 6 Air-to-air missile R-27, RVV-AE and R-27T or 4 x R-73. Anti-ship missile Moskit. |
