Air Power Series>1:72 die-cast display model>Su-25>HA6109
Su-25K Frogfoot 25616, 114 Sqn., Iraqi Air Force, 1991
General Background
In 1999 Russia decided to upgrade their aging Su-25 aircraft with actual work beginning in 2001.
The first of the upgraded aircraft designated Su-25SM (Stroyevoy Modernizirovannyi) Grach
(Rook) flew on March 3, 2002 with the first six modernized aircraft entering service with the
Russian Air Force in December 2006. The idea behind the modernization was to expand the life
of the Su-25, make it All-Weather capable, more lethal and reduce operating and maintenance
cost. Increased ordnance loads and a wider selection were also added.
The Aircraft
Early into the Iran-Iraq War Iraq approached Russia to purchase various types of military equipment and one such item was the Su-25 Frogfoot. Iraq became the first non Warsaw Pact country to be equipped with the Su-25K and Su-25UBK. They received 69 Su-25Ks and 4 Su-25UBK trainers. The first operational Iraqi regiment was ready in 1986. During Operation Desert Storm none of the Su-25s were a threat to Allied forces. A few would seek refuge in Iran while others were buried in the desert sand and several were destroyed in their hardened bunkers.
Specifications :
Manufacturer: | Sukhoi Design Bureau |
Role: | Close Air Support (CAS) |
Number Built: | 1024 |
User Countries: | Approximately 28 |
Crew: | 1 Pilot |
Dimensions | |
Length: | 15.53 m (51 ft) including nose probe |
Wingspan: | 14.3 m (47 ft 2 in) |
Height: | 4.8 m (15 ft 9 in) |
Weight: | |
Empty: | 9,800 kg (21,605 lbs) |
Normal Takeoff : | 14,400 kg (31,835 lbs) |
Maximum Takeoff: | 19,300 kg (42,549 lbs) |
Performance | |
Power Plant: | 2 X Soyuz/Tumansky R-195 Turbojets Producing 44.18 kN (9,921 lbf) Per Engine |
Maximum speed: | Mach .079 (975 km/h) (606 mph) @ Sea Level |
Rate Of Climb: | 58 m/s (11,400 ft/min) |
Service Ceiling | |
Clean: | 7,000 m (23,000 ft) |
With Ordnance: | 5,000 m (16,000 ft) |
Range: | Cruise Clean @ Altitude – 1,000 km (621 nmi) |
Combat Range | 750 km (405 nmi) @ Sea Level With 4,400 kg (9,700 lbs) Of Ordnance and 2 External Fuel Tank |
Maximum G-Load: | 6.5 g+ |
Armament: | |
Gun: | 1 X 30 mm Gryazev-Shipunov GSh-30-2 Auto-Cannon With 250 Rounds SPPU-22 Gun Pods To House 2 X 23 mm Gryazev-Shipunov GSh-23 Auto-Cannons With 260 Rounds |
Hardpoints: | 11 For Maximum Load of 4,400 kg (9,700 lbs) Of Various Combinations
Rockets UB-32A Rocket Pods For S-5 Rockets B-8M1 Rocket Pods For S-8 Rockets S-13 S-24 S-25 Missiles Air-To-Air K-13A R-60 R-73E Air-To-Surface Kh-23 Kh-25ML Kh-29L Anti-Radiation Kh-28 Bombs FAB-250 GPB FAB-500 GPB KAB-500K TV-Guided ZB-500 Incendiary |
Other: | ASO-2V Chaff and Flare Dispensers
Some Su-25 Deployed in Syria Carried 4 Rows of ASO-2V Dispensers Along Upper Tail Cone Surface Behind Vertical Stabilizer |
Radar: | Phazoton Kopyo |