Su-25UBM Frogfoot Attack aircraftt. First flight: 2008 © Konstantinos Panitsidis

Photos from the personal collection of Konstantinos Panitsidis


 Technical Specifications      Photos      Video

 

 

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

DESIGNER
OKB Sukhoi
COUNTRY
Russia
TYPE
Attack aircraft
CREW
2
POWER-PLANT
Two jet, R-95Sh
Thrust, kg
2 x 4.100
DIMENSIONS
 
Length, m
15,36
Height, m
5,20
Wing span, m
14,36
Wing area, m2
30,10
WEIGHT
 
Empty aircraft, kg
10.030
Normal take-off, kg
15.300
Maximum take-off, kg
17.600
Internal fuel, kg
2.750
PERFORMANCE
 
Maximum speed, km/h
860
Max speed in low height, km/h
970
Combat range, km
950
- low height, km 450
Range, km 2.400
Service ceiling, m
7.000-10.000
Maximum overload, g
6.5
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.

 


PHOTOS Su-25UBM