In numbers Through the lens Video
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
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
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. |