Su-25 Grach Attack aircraft

Su-25 Grach Attack aircraft. First flight: 1975 © Konstantinos Panitsidis
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NATO reporting name: Frogfoot
Russian name: Grach (named after Rock (bird))

 

A single-seat subsonic armoured attack aircraft powered by two R-95Sh 4,100-kgf turbojet engines. The Su-25 prototype powered by R9-300 engines made its maiden flight on 22 February, 1975. Since 1979, the aircraft has been under series production at the Tbilisi aircraft plant. 

In 1985, a twin-seat version production was started at the Ulan-Ude plant. Since the mid-nineties, that plant has been building single-seat variants too. By 2001, a total of over 1,300 Su-25s in all versions have been made.

Su-25 Grach, MAKS-2007 © Konstantinos Panitsidis

Su-25 Grach, MAKS-2007 © Konstantinos Panitsidis

 

The Su-25 served as the basis for deriving the following variants: 
the Su-25UB twin-seat combat trainer whose maiden flight was made on 10 August 1985.
Su-25UT (Su-28) twinseat trainer carrying no weapons (1987).
Su-25BM target hauler (1990).
Su-25T single-seat attack aircraft fitted with the Shkval sight and Vikhr ATGM system (its maiden flight was made on 17 August, 1984).

Su-25K and Su-25UBK export versions of the Su-25 and Su-25UB (exported to Angola, Iraq, the PDRK and Czechoslovakia during 1984-1989). 

In 2001, an upgrade programme for Russian Air Force Su-25 and Su-25UB attack aircraft was launched. Modernised Su-25SM singleseat attack aircraft will be retrofitted with a novel sight/navigation suite comprising an advanced digital computer, a LCD-based cockpit management system, a satellite navigation receiver and an uprated radionavigation equipment. This will result in enhanced navigation and attack accuracy.


Su-25UTG, MAKS-2007 © Konstantinos Panitsidis
Su-25UTG, MAKS-2007 © Konstantinos Panitsidis

 

The Su-25UBM twinseat upgrade is going to receive in addition the Kopyo radar to step up its combat capabilities.

 


Technical specifications

DESIGNER OKB Sukhoi
COUNTRY Russia
TYPE
Attack aircraft
CREW 1
POWER-PLANT Two turbojet engines R-195
Thrust, kgf 2x4.500
DIMENSIONS  
Length, m 15,36
Height, m 4,80
Wing span, m 14,36
Wing area, m2 33,70
WEIGHT  
Maximum take-off, kg 17.600
Normal take-off, kg 14.600
Empty aircraft, kg 9.500
Internal fuel, kg 5.000
Weight of transported fuel with external tanks, kg 2.000
Warload, kg 4.340
PERFORMANCE  
Maximum speed (at high altitude), km/h 1.004
Maximum speed, sea level km/h -
Maximum speed in low height, km/h 975
Range, km 1.850
Combat range, km  
- at high altitude 1.250
- in low height 750
Service ceiling, m 7.000-10.000
Maximum overload, g 6,5
ARMAMENT 30 mm two-barrel cannon GSh-30-2 with 250 rounds. Number external hardpoints: 8 (10). Transportation of weapons: 8-10x500, 250 kg bombs, 32x100 kg bombs, napalm tanks, rokets 8-10 ML UB-32-57 (320 (252)x57 mm) or 8-10 240 mm, packets UR S-5 (57 mm), S-8 (80 mm), S-24 (240 mm)xS-25 (340 mm).
Air-to-air missile, Air-to-surface missile Kh-25ML, Kh-29L and S-5L. SPPU-22 pods with 23-mm cannon GSh-23L with 260 rounds.