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MiG-29UBT
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The MiG-29UBT is a twin-seat multirole combat aircraft derived from the MiG-29UB combat trainer powered by two RD-33 engines 8,300-kgf each. In developing the MiG-29UBT, the same principle were employed, that had been used in upgrading the MiG-29 singleseater under the MiG-29SMT programme, namely an open-architecture avionics suite, an electronic indication system, advanced weapons systems including air-to-surface guided weapons, a mid-air refuelling system, etc. the MiG-29UBT's fire control system is wrapped around the small-size Osa-2 multifunctional phased-array radar. 

 

MiG-29UBT airplane with Kh-29 guided missile

MiG-29UBT airplane with Kh-29 guided missile.


The first MiG-29UBT prototype was built by the Mikoyan design bureau in May 1998 and accomplished its maiden flight on 24 August that same year. The spring 1999 saw the second MiG-29UBT flying prototype assembly completed in cooperation with the Sokol aircraft production plant. The second prototype flew on 26 May, 1999.

 

MiG-29UBT of later production series.

MiG-29UBT of later production series.

 

The first MiG-29UBTs joined the Russia AF in 2004, as a modernized two-seat multirole combat aircraft (training fighter). All "UBT" do not have radar (Osa-2), while they were equipped with a collapsible fuel refueling tube, without the ability to take fuel in the air (s.s. its use is possible only for training in air refueling).

 

 


Three-view drawing

MiG-29UBT © Konstantinos Panitsidis

 

 


Technical specifications

DESIGNER OKB MiG
COUNTRY Russia
TYPE
Twin-seat multirole combat aircraft (training fighter)
CREW 2
POWER-PLANT Two tutbofan bypass engines RD-33
Thrust, kgf 2x8.300
DIMENSIONS  
Length, m 15,95
Length+Pitot, m 17,42
Height, m 4,73
Wing span, m 11,36
Wing area, m2 31,80
WEIGHT  
Maximum take-off, kg 21.000
Normal take-off, kg 16.800
Empty aircraft, kg 12.100
Internal fuel, kg -
Weight of transported fuel with external tanks, kg -
Warload, kg up to 5.000
PERFORMANCE  
Maximum speed, km/h 2.230
Maximum speed in low height, km/h 1.500
Range in low height, km 680
Range in high altitude, km 1.410
Range at high altitude, with external fuel tanks, km 2.000
Service ceiling, m 17.500
Rate of climb, m/min -
Maximum overload, g 9
ARMAMENT
1x30 mm cannon GSh-301. Number external hardpoints: 6 (7). Transportation of weapons: AAM R-27R, R-27T, R-27ER, R-27ET, RVV-AE and R-73, ASM Kh-29L, Kh-29T and Kh-59M, anti-ship missiles Kh-31A and  Kh-31U,  anti-radar ASM Kh-31P, 500 kg bombs KAB and free fall bombs.