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| Country:
USSR |
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Type: Close air support |
| Manufacturer:
Sukhoi |
| Service:
1981 - 2008 |
| First
Flight: 22 February 1975 |
| Production:
1024 |
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The Sukhoi Su-25 is a single-seat, twin-engine jet aircraft developed in the Soviet Union by the Sukhoi Design Bureau. It was designed to provide close air support for the Soviet Ground Forces. The first prototype made its maiden flight on 22 February 1975. After testing, the aircraft went into series production in 1978 at Tbilisi in the Soviet Republic of Georgia. NATO assigned the new aircraft the reporting name Frogfoot.
Early variants included the Su-25UB two-seat trainer, the Su-25BM for target-towing, and the Su-25K for export customers. Upgraded variants developed by Sukhoi include the Su-25T and the further improved Su-25TM (also known as Su-39). By year 2007, the Su-25 is the only armoured airplane still in production except the Su-34 whose production just started. It is currently in service with Russia and various other CIS states as well as export customers.
During its more than twenty-five years in service, the Su-25 has seen combat with several air forces. It was heavily involved in the Soviet war in Afghanistan, flying counter-insurgency missions against the Mujahideen. The Iraqi Air Force employed Su-25s against Iran during the 1980“89 Iran“Iraq War. Most of them were later destroyed or fled to Iran in the 1991 Gulf War. In 1993, Abkhazian separatists used Su-25s against Georgians during Abkhazian War. Eight years later, the Macedonian Air Force employed Su-25s against Albanian insurgents in the 2001 Macedonia conflict, and in 2008 Georgia and Russia were both reported to be using Su-25s in the 2008 South Ossetia War.
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| TECHNICAL
SPECIFICATIONS ( Su-25TM) |
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General characteristics
- Crew: one pilot
- Length: 15.33 m (50 ft 11)
- Wingspan: 14.36 m (47 ft 1 in)
- Height: 4.80 m (15 ft 9 in)
- Wing area: 30.1 m (324 ft)
- Empty weight: 10,740 kg (23,677 lb)
- Loaded weight: 16,990 kg (37,456 lb)
- Max takeoff weight: 20,500 kg (45,194 lb)
- Powerplant: 2 x Tumansky R-195 turbojets, 44.18 kN (9,480 lbf) each
Performance
- Maximum speed: 950 km/h (590 mph, Mach 0.82)
- Combat radius: 375 km (235 mi)
- Ferry range: 2,500 km (1,553 mi)
- Service ceiling 10,000 m (22,200 ft)
- Rate of climb: 58 m/s (11,400 ft/min)
- Wing loading: 584 kg/m (119 lb/ft)
- Thrust/weight: 0.51
Armament
- 1 x GSh-30-2 30mm cannon with 250 rounds
- 11 hardpoints for up to 4,400 kg (9,700 lb) of disposable ordnance, including rails for two R-60 (AA-8 'Aphid') or other air-to-air missiles for self-defence and a wide variety of general-purpose bombs, cluster bombs, gun pods, rocket pods, laser-guided bombs, and air-to-surface missiles such as the Kh-25ML
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