Su-25UTG Frogfoot Training aircraft, MAKS-2007 © Konstantinos Panitsidis

Photo from the personal collection of Kostas Panitsidis


 Technical specifications      Photos      Video

 

 

A twin-seat carrier-based combat trainer powered by two R-95Sh turbojet engines each producing 4,100-kgf thrust. 

The Su-25UTG is a derivative of the Su-25UB combat trainer version of the baseline Su-25 attack aircraft. It differs from the Su-25UB in having the arrestor hook for practising flying off and on the deck of the aircraft carrier as well as a somewhat lighter airframe due to the fact that its weaponry and armour plates were dismounted. 

The Su-25UTG made its maiden flight in September 1988, with its production beginning in 1990 at the Ulan-Ude plant. A total of a dozen aircraft have been manufactured to date. 

The Su-25UTG is operated by the composite air division deployed on the Admiral Kuznetsov aircraft carrier. In 1999, one of the aircraft was fitted with a folding wing.

 


TECHNICAL SPECIFICATIONS

DESIGNER
OKB Sukhoi
COUNTRY
Russia
TYPE
Training aircraft
CREW
2
POWER-PLANT
Two jet, R-195Sh
Thrust, kN
2 x 44.13
DIMENSIONS
 
Length, m
15,36
Height, m
4,80
Wing span, m
14,36
Wing area, m2
33,70
WEIGHT
 
Empty aircraft, kg
9.500
Normal take-off, kg
14.600
Maximum take-off, kg
17.600
Internal fuel, kg
5.000
PERFORMANCE
 
Maximum speed, km/h
Μ=0,82
Max speed in low height, km/h
975
Combat range, km
625
Service ceiling, m
7.000-10.000
Maximum overload, g
6.5
ARMAMENT -