.jpg "Su-25UBM Frogfoot Attack aircraftt. First flight: 2008 © Konstantinos Panitsidis")
Photos from the personal collection of Konstantinos Panitsidis
Technical Specifications 
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The first prototype of training multiple role fighter Su-25UBM was completed in 2007, developed by Aviation factory Ulan-Ude and was first presented at MAKS-2007, where itcaused increased interest from representatives of the Ministry of Defence and foreign countries.
The modernized version of Su-25UBM was developed on the basis of the Su-25UB (Training - near support).
The Su-25UBM is equipped with new radar type Phazatron NII Kopyo, new target system Bars, new weapon systems, automatic delivery systems and self-protection. The first flight of the prototype took place in 2008.
The modernized Su-25UBM is considered equivalent to Su-25SM.
Production will begin in mid 2012 (according to the timetable of the Armed Forces 2012 to 2020), and is expected to last until 2020.
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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Attack aircraft
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CREW
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2
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POWER-PLANT
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Two jet, R-95Sh
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Thrust, kg
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2 x 4.100
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DIMENSIONS
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Length, m
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15,36
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Height, m
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5,20
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Wing span, m
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14,36
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Wing area, m2
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30,10
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WEIGHT
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Empty aircraft, kg
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10.030
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Normal take-off, kg
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15.300
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Maximum take-off, kg
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17.600
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Internal fuel, kg
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2.750
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PERFORMANCE
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Maximum speed, km/h
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860
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Max speed in low height, km/h
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970
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Combat range, km
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950
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| - low height, km | 450 |
| Range, km | 2.400 |
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Service ceiling, m
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7.000-10.000
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Maximum overload, g
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6.5
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| ARMAMENT | 30 mm two-barrel cannon GSh-30-2 with 250 rounds. Warload - 4.340 kg in 8 (10) hardpoints, normal -1.340 kg Air-to-air missile R-60, R-27R(E), RVVE-AE (R-77) or R-73. 8-10 x 500,250 kg bombs, 32 x 100 kg bombs, napalm tanks, rokets 8-10 x ML , UB-32-57 (320(252) x 57 mm) or 8-10 240 mm, packets UR S-5 (57 mm), S-8 (80 mm), S-24 (240 mm) x S-25 (340 mm). Air-to-air missile, Air-to-surface missile Kh-25ML, Kh-29L and S-25L. SPPU-22 pods with 23 mm cannon GSh-23L with 260 rounds. |
