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Sukhoi Su-25
Sukhoi Su-25
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The Sukhoi Su-25 Grach (Russian: Грач (rook); NATO reporting name: Frogfoot) is a subsonic, single-seat, twin-engine jet aircraft developed in the Soviet Union by Sukhoi. It was designed to provide close air support for Soviet Ground Forces. The first prototype made its maiden flight on 22 February 1975. After testing, the aircraft went into series production in 1978 in Tbilisi in the Georgian Soviet Socialist Republic.

Key Information

Early variants included the Su-25UB two-seat trainer, the Su-25BM for target-towing, and the Su-25K for export customers. Some aircraft were upgraded to the Su-25SM standard in 2012. The Su-25T and the Su-25TM (also known as the Su-39) were further developments, not produced in significant numbers. The Su-25, and the Su-34, were the only armoured, fixed-wing aircraft in production in 2007.[1] Su-25s are in service with Russia, other CIS members, and export customers. Production of the Su-25 ended in 2010 in Georgia.[2] Attempts continue to be made to restart production in Georgia using partially completed airframes,[3] but as of June 2022 no new deliveries have been reported.

Since entering service more than 44 years ago, the Su-25 has seen combat in several conflicts. The type was heavily involved in the Soviet–Afghan War, flying counter-insurgency missions against the Afghan Mujahideen. The Iraqi Air Force employed it against Iran during the 1980–88 Iran–Iraq War. Most Iraqi examples were later destroyed or flown to Iran in the 1991 Persian Gulf War. The Georgian Air Force used Su-25s during the Abkhazian war from 1992 to 1993. The Macedonian Air Force used Su-25s against Albanian insurgents in the 2001 Macedonian conflict and, in 2008, Georgia and Russia both used Su-25s in the Russo-Georgian War. African states, including the Ivory Coast, Chad, and Sudan have used the Su-25 in local insurgencies and civil wars. Recently, the Su-25 has seen service in the Russian intervention in the Syrian civil war, the clashes of the 2020 Nagorno-Karabakh War, and on both sides in the Russian invasion of Ukraine.[4]

Development

[edit]

In early 1968, the Soviet Ministry of Defence decided to develop a specialised shturmovik armoured assault aircraft in order to provide close air support for the Soviet Ground Forces. The idea of creating a ground-support aircraft came about after analysing the experience of ground-attack (shturmovaya) aviation during the 1940s, 1950s, and 1960s.[5] The Soviet fighter-bombers in service or under development at the time (Su-7, Su-17, MiG-21 and MiG-23) did not meet the requirements for close air support of the army.[5] They lacked essential armour plating to protect the pilot and vital equipment from ground fire and missile hits, and their high flight speeds made it difficult for the pilot to maintain visual contact with a target. Having taken into account these problems, Pavel Sukhoi and a group of leading specialists in the Sukhoi Design Bureau started preliminary design work in a comparatively short period of time, with the assistance of leading institutes of the Ministry of the Aviation Industry and the Ministry of Defence.[6]

This Su-25UB of the Ukrainian Air Force is a two-seater version intended for both combat and training.

In March 1969, a competition was announced by the Soviet Air Force that called for designs for a new battlefield close-support aircraft. Participants in the competition were the Sukhoi design bureau and the design bureaus of Yakovlev, Ilyushin and Mikoyan.[7] Sukhoi finalised its "T-8" design in late 1968, and began work on the first two prototypes (T8-1 and T8-2) in January 1972. The T8-1, the first airframe to be assembled, was completed on 9 May 1974. Another source says November 1974. However, it did not make its first flight until 22 February 1975, after a long series of test flights by Vladimir Ilyushin[citation needed]. The Su-25 surpassed its main competitor in the Soviet Air Force competition, the Ilyushin Il-102, and series production was announced by the Ministry of Defence.[8][9]

During flight-testing phases of the T8-1 and T8-2 prototypes' development, the Sukhoi Design Bureau's management proposed that the series production of the Su-25 should start at Factory No. 31 in Tbilisi, Soviet Republic of Georgia, which at that time was the major manufacturing base for the MiG-21UM "Mongol-B" trainer. After negotiations and completion of all stages of the state trials, the Soviet Ministry of Aircraft Production authorised manufacture of the Su-25 at Tbilisi, allowing series production to start in 1978.[10]

In the late 1980s and early 1990s, several Su-25 variants appeared, including modernised versions, and variants for specialised roles. The most significant designs were the Su-25UB dual-seat trainer, the Su-25BM target-towing variant, and the Su-25T for antitank missions. In addition, an Su-25KM prototype was developed by Georgia in co-operation with Israeli company Elbit Systems in 2001, but so far this variant has not achieved much commercial success. As of 2007, the Su-25 was the only armoured aircraft still in production.[1]

The Russian Aerospace Forces, which operates the largest number of Su-25s, planned to upgrade older aircraft to the Su-25SM variant, but funding shortfalls had slowed the progress; by early 2007 only seven aircraft had been modified.[11]

Design

[edit]

The Su-25 has a conventional aerodynamic layout with a shoulder-mounted trapezoidal wing and a traditional tailplane and rudder. Several metals are used in the construction of the airframe: 60% aluminium, 19% steel, 13.5% titanium, 2% magnesium alloy and 5.5% other materials.[12]

Su-25 at Kubinka air base

All versions of the Su-25 have a metal cantilever wing, of moderate sweep, high aspect ratio and equipped with high-lift devices. The wing consists of two cantilever sections attached to a central torsion box, forming a single unit with the fuselage. The air brakes are housed in fairings at the tip of each wing. Each wing has five hardpoints for weapons carriage, with the attachment points mounted on load-bearing ribs and spars.[13] Each wing also features a five-section leading edge slat, a two-section flap and an aileron.

The flaps are mounted by steel sliders and rollers, attached to brackets on the rear spar. The trapezoidal ailerons are near the wingtips.[14] The fuselage of the Su-25 has an ellipsoidal section and is of semi-monocoque, stressed-skin construction, arranged as a longitudinal load-bearing framework of longerons, beams and stringers, with a transverse load-bearing assembly of frames.[12] The one-piece horizontal tailplane is attached to the load-bearing frame at two mounting points.[14]

Early versions of the Su-25 were equipped with two R-95Sh non-afterburning turbojets, in compartments on either side of the rear fuselage. The engines, sub-assemblies and surrounding fuselage are cooled by air provided by the cold air intakes on top of the engine nacelles. A drainage system collects oil, hydraulic fluid residues and fuel from the engines after flight or after an unsuccessful start. The engine control systems allows independent operation of each engine.[14] The latest versions (Su-25T and TM) are equipped with improved R-195 engines.[15]

Nose view of the Su-25

The autocannon is in a compartment beneath the cockpit, mounted on a load-bearing beam attached to the cockpit floor and the forward fuselage support structure. The nose is fitted with distinctive twin pitot probes and hinges up for service access.[12]

Cockpit

[edit]
Cockpit

The pilot flies the aircraft by means of a centre stick and left hand throttles. The pilot sits on a Zvezda K-36 ejection seat (similar to the Sukhoi Su-27) and has standard flight instruments. At the rear of the cockpit is a six-millimetre-thick (0.24 in) steel headrest, mounted on the rear bulkhead. The cockpit has a bathtub-shaped armoured enclosure of welded titanium sheets, with transit ports in the walls. Guide rails for the ejection seat are mounted on the rear wall of the cockpit.[12]

The canopy hinges open to the right and the pilot enters using the flip-down ladder. Once inside, the pilot sits low in the cockpit, protected by the bathtub assembly, which makes for a cramped cockpit. Visibility from the cockpit is limited, being a trade-off for improved pilot protection. Rearwards visibility is poor and a periscope is fitted on top of the canopy to compensate.[16]

A folding ladder built into the left fuselage provides access to the cockpit as well as to the top of the aircraft.

Avionics

[edit]

The base model Su-25 incorporates a number of key avionics systems. It has no TV guidance but includes a distinctive nose-mounted laser rangefinder that is thought to provide for laser-based target finding.[16][17] A DISS-7 doppler radar is used for navigation; the Su-25 can fly at night, in visual and instrument meteorological conditions.

The Su-25 often has radios installed for air-to-ground and air-to-air communications, including an SO-69 identification-friend-or-foe (IFF) transponder. The aircraft's self-defence suite includes various measures, such as flare and chaff dispensers capable of launching up to 250 flares and dipole chaff. Hostile radar uses are guarded against via an SPO-15 radar warning receiver.

An airtight avionics compartment is behind the cockpit and in front of the forward fuel tank.

The newer Su-25TM and Su-25SM models have an upgraded avionics and weapons suite, resulting in improved survivability and combat capability.[18]

Operational history

[edit]

Soviet–Afghan War

[edit]

The first Soviet Air Force Su-25 unit was the 80th Assault Aviation Regiment, formed in February 1981 based at Sitalcay air base in the Azerbaijan Soviet Socialist Republic.[19] The first eleven aircraft arrived at Sitalchay in May 1981.[20] The 200th Independent Assault Aviation Squadron was then formed within the regiment to go to Afghanistan.

On 19 July 1981, the 200th Independent Attack Squadron was reassigned to Shindand Airbase in western Afghanistan, becoming the first Su-25 unit deployed to that country. Its main task was to conduct air strikes against mountain military positions and structures controlled by the Afghan rebels.[21] Another Soviet Su-25 unit was the 368th Assault Aviation Regiment, which was formed on 12 July 1984, at Zhovtneve in Ukraine.[22] It was soon also moved east to conduct operations over Afghanistan.

Over the course of the Soviet–Afghan War, Su-25s launched 139 guided missiles of all types against Mujahideen positions. On average, each aircraft performed 360 sorties a year, a total considerably higher than that of any other combat aircraft in Afghanistan. By the end of the war, nearly 50 Su-25s were deployed at Afghan airbases, carrying out a total of 60,000 sorties. Between the first deployment in 1981 and the end of the war in 1989, 21–23 aircraft were lost in combat operations, with up to nine destroyed on the ground while parked.[21][23]

Iran–Iraq War

[edit]

The Su-25 also saw combat during the Iran–Iraq War of 1980–88. The first Su-25s were commissioned by the Iraqi Air Force in 1987 and performed approximately 900 combat sorties towards the end of the war, carrying out the bulk of Iraqi air attack missions. During the most intense combat of the war, Iraqi Su-25s performed up to 15 sorties per day, each. In one recorded incident, an Iraqi Su-25 was shot down by an Iranian, Hawk surface-to-air missile, but the pilot managed to eject. This was the only confirmed, successful Iranian shootdown of an Iraqi Su-25. After the war, Saddam Hussein decorated all of the Iraqi Air Force's Su-25 pilots with the country's highest military decoration.[21]

Gulf War

[edit]
An Iraqi Su-25 destroyed during Operation Desert Storm

During the Gulf War of 1991, the air superiority of the coalition forces was so great that the majority of Iraqi Su-25s did not even manage to get airborne. On 25 January 1991, seven Iraqi Air Force Su-25s fled from Iraq and landed in Iran.[24]

On the evening of 6 February 1991, two US Air Force F-15C Eagle fighters of the 53rd Tactical Fighter Squadron, operating from Al Kharj Air Base in Saudi Arabia, intercepted a pair of Iraqi MiG-21s and a pair of Su-25s. All four Iraqi aircraft were shot down, with both Su-25s coming down in the desert not far from the Iraqi border with Iran. This was the Iraqi Su-25s' only air combat of the war.[21]

Abkhazian War

[edit]

The Georgian government used Su-25s in 1992–93 against Abkhaz separatists during the First Abkhazian War.[25] A Georgian Air Force Su-25 was shot down over Nizhnaya Eshera on 4 July 1993 by an 9K34 Strela-3 MANPADS.[26][27] Another Georgian Su-25 was shot down on 13 July 1993 with a 9K32 Strela-2 MANPADS,[28] while another Su-25 was downed by friendly fire by a ZU-23-2 on 4 July.[28] The Russian Air Force also lost an Su-25 during war, the aircraft crashed due to a pilot's mistake while providing CAS for Abkhaz forces.[28]

First Chechen War

[edit]

Russian Su-25s were employed during the First Chechen War. Together with other Russian Air Force air assets, they achieved air supremacy for Russian Forces. On 29 November 1994, attacking all four Chechen military bases, Russian Su-25 from the 368th Assault Aviation Regiment (OShAP) destroyed up to 266 Chechen aircraft on the ground, mostly not airworthy.[29] The Air Force's deployed assets performed around 9,000 air sorties, with around 5,300 being strike sorties during the Chechen campaign between 1994 and 1996. The Russian 4th Air Army had 140 Sukhoi Su-17Ms, Su-24s and Su-25s in the war zone supported by an A-50 AWACS aircraft. The employed munitions were generally unguided S-5, S-8, and S-24 rockets, as well as FAB-250 and FAB-500 bombs, while only 2.3% of the strikes used precision-guided Kh-25ML missiles, KAB-500L and KAB-500KR smart bombs when weather conditions were suitable.[30] Russian forces were not able to properly take advantage of the air supremacy due to obsolete air tactics that focused the Air Force on useless tasks in this type of war such as Combat Air Patrols.[31] The Russian air losses were low since no integrated air defense was fielded by the Chechens.[32]

On 4 February 1995, a Russian Su-25 was shot down by ZSU-23-4 Shilka antiaircraft fire over Belgatoi Gekhi, five kilometers southeast of Grozny. The pilot, Maj. Nikolay Bairov, ejected but died impacting the ground as his parachute did not deploy on time. Another Su-25 piloted by Lt. Col. Evgeny Derkulsky was damaged by ground fire on the same day, but managed to land at Mozdok air base, where the aircraft was repaired.[29] On 5 May 1995, another Russian Su-25 was downed near Serzhen-Yurt by 12.7 mm fire while on a low-altitude patrol. The pilot, Col. Vladimir Sarabeyev, was killed.[33]

On 4 April 1996, another Su-25 fell either to ZU-23-2 fire while either making a reconnaissance flight or attacking the village of Goiskoye. The pilot, Maj. Alexander Matvienko, ejected and was recovered by a friendly helicopter returning to the airbase in Khankala, Grozny.[34] On 5 May 1996, a two-seat Su-25UB was downed with an 9K34 Strela-3 MANPADS near the village of Mairtup while on reconnaissance. Both pilots, Col. Igor Sviryidov and Maj. Oleg Isayev, were killed in the crash. It was the fourth Su-25 shot down and fifth Russian fixed wing aircraft lost, since the start of the war in December 1994.[32][35]

Second Chechen War

[edit]

Russian Air Force Su-25s were extensively used during the Second Chechen War in particular during the first phase when Russian forces were invading the self-proclaimed Chechen Republic of Ichkeria.[36] Up to seven Russian Su-25s were lost,[32] one to hostile fire: on 4 October 1999, a Su-25 was shot down by a MANPADS during a reconnaissance mission over the village of Tolstoy-Yurt killing its pilot. The wings of the aircraft were put on a pedestal in the central square in Grozny.[34][37]

Ethiopian–Eritrean War

[edit]

Su-25 attack aircraft were used by the Ethiopian Air Force to strike Eritrean targets. On 15 May 2000, An Ethiopian Su-25 was shot down by an Eritrean Air Force MiG-29, killing the pilot.[38]

2001 insurgency in the Republic of Macedonia

[edit]

Su-25s were used by the Macedonian Air Force but flown by Ukrainian pilots during the conflict against Albanian separatists. Beginning on 24 June 2001, the aircraft made multiple attack runs against separatist positions. The Su-25s were only used during the Battle of Raduša on the last day.[39]

War in Darfur

[edit]

Sudan has used Su-25s in attacks on rebel targets and possibly civilians in Darfur.[40]

Ivorian-French clashes

[edit]

During the Ivorian Civil War, Su-25s were used by government forces to attack rebel targets. On 6 November 2004, at least one Ivorian Sukhoi Su-25 attacked a unit of France's Unicorn peacekeeping forces stationed in Bouaké, killing nine soldiers, a U.S. development worker and wounding 37 soldiers.[41] Shortly afterwards, the French military retaliated by attacking the air base in Yamoussoukro and destroyed the Ivorian air force, heavily damaging the two Su-25s responsible for the attack.[42][43]

2008 Russia–Georgia war

[edit]
A Russian Su-25

In August 2008, Su-25s were used by both Georgia and Russia during the 2008 Russia–Georgia war. Su-25s of the Georgian Air Force participated in providing air support for troops during Battle of Tskhinvali and launched bombing raids on targets in South Ossetia.[44] Russian military Su-25s struck Georgian forces in South Ossetia, and undertook air raids on targets in Georgia.[45] The Russian military officially confirmed the loss of three Su-25 aircraft to the Georgian air defense, though the Moscow Defense Brief suggests four.[46][47] The three Russian aircraft were reportedly downed by Georgian Buk-M1 air defence units.[48] Georgian Su-25s were able to operate at night.[48] In early August 2008, Russian Su-25s attacked the Tbilisi Aircraft Manufacturing plant, where the Su-25 is produced, dropping bombs on the factory's airfield.[49]

Iran

[edit]

On 1 November 2012, two Iranian Su-25s fired cannon bursts at a USAF MQ-1 Predator drone 30 km (19 mi; 16 nmi) off the Iranian coast. The Iranian government has claimed that the drone violated its airspace.[50][51][52]

War in Donbas

[edit]
Sukhoi Su-25s of the Ukrainian Air Force in 2013

Ukrainian armed forces deployed aircraft over insurgent Eastern regions starting in spring 2014. On 26 May 2014, Ukrainian Su-25s supported Mi-24 helicopters during a military operation to regain control over the airport in Donetsk, during which the Su-25s fired air to ground rockets.[53] On 2 July 2014, one Ukrainian Su-25 crashed due to a technical fault.[54][55]

On 16 July 2014, an Su-25 was shot down, with Ukrainian officials stating that a Russian MiG-29 shot it down using a R-27T missile.[56][57] Russia denied these allegations.[58]

On 23 July 2014, two Su-25s were shot down in the Donetsk region of Ukraine. A spokesperson for the National Security and Defense Council of Ukraine said the aircraft were shot down by missiles fired from Russia.[59]

On 29 August 2014, a Ukrainian Su-25 was shot down by pro-Russian rebels. The Ukrainian authorities said the downing was due to a Russian missile without clarifying if they mean Russian made or fired by Russian forces. The pilot managed to eject safely. On the same day, pro-Russian rebels claimed the downing of up to four Su-25s.[60][61]

On 9 February 2015, the pro-Russian forces indirectly acknowledged, for the first time, with a reference to a Ukrainian media source, their use of Su-25 against Ukrainian forces during the fighting near Debaltsevo.[62]

2014 Northern Iraq offensive

[edit]
An Iraqi Air Force Su-25

On 29 June 2014, it was reported that Iraq claimed to have received the first batch of second hand Su-25s ordered from Russia in order to fight Islamic State forces. An Iraqi defense ministry source claimed the aircraft would be in service "within three to four days", despite the fact that the Iraqis require technical help and parts to make them operational, and the fact that the Russian made aircraft are incompatible with the Iraqi Air force's inventory of American made Hellfire missiles.[63][64]

The Islamic Revolutionary Guards Corps Air Force delivered seven Su-25s on 1 July 2014, the majority of which were ex-Iraqi aircraft from the Gulf War.[65] They were quickly pushed into combat, performing air raids as early as the beginning of August 2014 and later expanding their area of operation.[66][67]

Iraqi Su-25s flew the bulk of the sorties against the Islamic State, with 3562 missions between June 2014 and December 2017, by which time ISIS had lost control of all the territory it formerly controlled in Iraq. That compares to 514 sorties flown by the Iraqi fleet of F-16IQ fighters.[68]

Russian military intervention in Syria

[edit]

In September 2015, it was reported that at least a dozen Su-25 were deployed by Russia to an airfield near Latakia, Syria, to support the Russian forces there who were taking part in the Syrian offensive against ISIL.[69] On 2 October 2015, Russian Su-24M and Su-25 attack aircraft destroyed an ISIL command post in the Idlib province, while Su-34 and Su-25 aircraft eliminated an ISIL fortified bunker in the Hama province.[citation needed] By 15 March 2016, with the scaling down of Russian presence in Syria, Russian Su-25s had performed over 1,600 sorties in Syria while dropping 6,000 bombs.[70]

On 3 February 2018 a Russian Su-25 was shot down over Idlib by rebel fighters who used a MANPADS. A Syrian militant said that the pilot, Roman Filipov, ejected safely but killed himself with a grenade to avoid capture.[71][72][73][74]

2020 Nagorno-Karabakh War

[edit]
An Azerbaijani Su-25 in 2022

On 29 September 2020, Armenian Defense Ministry claimed that an Armenian Air Force Su-25 was shot down by a Turkish Air Force F-16, killing the pilot. However Turkey denied the allegation.[75][76][77]

On 4 October 2020, an Azerbaijani Air force Su-25 aircraft was shot down, by Armenian forces, probably with a 9K33 Osa while targeting Armenian positions in Fuzuli. The pilot, Col. Zaur Nudiraliyev died in the crash. Azerbaijani officials acknowledged the loss in December 2020,[78][79] while disclosing a major role of crewed aviation being hidden during the active phase of the conflict with more than 600 airstrikes by crewed aviation from 27 September 2020 to 9 November 2020, with the Su-25 fleet, tasked with the critical role of suppression and destruction of the enemy air defense among others.[80]

2022 Russian invasion of Ukraine

[edit]

Russian service

[edit]

On 24 February 2022, Russia reported the loss of an Su-25 due to "pilot error."[81] On 1 March, a Russian Su-25SM was lost over Ukraine.[82][83] The next day, another Russian Su-25SM, registration number RF-91961 - Red 07, was shot down in Makariv, Ukraine.[84] On 4 March, two Russian Su-25SMs, the first with registration number RF-93026, were lost over Volnovakha, Ukraine. The second, with callsign Red 04, was lost along with its pilot.[85] Images of the aircraft wrecks were displayed on social media.[86] On 7 March, an Su-25 was lost during a combat mission in Ukraine.[87][88] On 10 March, one Su-25 with registration number RF-91969 was shot down near Kyiv and the pilot killed.[89][90] On 14 March, a Russian Su-25 was damaged by enemy fire, likely MANPADs, but managed to return to its base.[91] On 24 May Ukraine claimed to have shot down retired Major General Kanamat Botashev flying an Su-25 using a Stinger missile. It was unknown if he was in service, or a private military contractor.[92]

On 22 October 2023, Ukraine claimed to have shot down five Russian Su-25s, over the preceding ten days, during fighting in Donetsk.[93]

In late April 2024, Su-25s were flying unimpeded over Chasiv Yar, which, according to military analyst Rob Lee, indicated “a clear sign of a lack of Ukrainian air defense ammunition.”[94]

On 4 May 2024, the 110th Mechanized Brigade (Ukraine) claimed to have shot down a Su-25 over Donetsk Oblast.[95]

As of October 24, 2025, Russia has been visually confirmed to have lost at least 40 Su-25s (38 destroyed, 2 damaged).[96]


On June 13, 2025, an Su-25 was captured on video using unguided rocket to get the type's first air-to-air kill, another Su-25, flown by the pilot's wingman in the friendly fire accident[97]

Ukrainian service

[edit]
Ukrainian Su-25s performing a flypast during the Kyiv Independence Day Parade on 24 August 2021
Ukrainian Air Force Sukhoi Su-25 in 2023

The Ukrainian Air force also operates Su-25s. On 26 February 2022 three Su-25s from the 299th Tactical Aviation Brigade were lost. "Blue 19" and "Blue 30" were shot down over the Kherson region.[98] The pilots were presumed dead. Photos of the wrecks of the two Ukrainian aircraft were published.[99][100][101] A third aircraft from the 299th was lost, but the pilot was captured by Russian forces.[102] Ukrainian media acknowledged that the pilot was Ukrainian.[103] The next day another Su-25, "Blue 39", was shot down near Hlibivka Vyshgorod, Kyiv region.[104][105] On 2 March, one Su-25 from 299th Tactical Aviation Brigade piloted by Oleksandr Korpan was lost over Starokostiantyniv, Khmelnytskyi Oblast.[106][107][108] On 10 March one Su-25, "Blue 31" was shot down near Nova Kakhovka, Kherson.[109][110][111] On 14 March another Su-25 was shot down by Russian forces in Volnovakha, Donbas region. The pilot was captured by Russian forces and later released on 24 April, in a Russo-Ukrainian prisoner swap.[112][113] On 22 March, a Ukrainian Su-25, heavily damaged in combat was recorded in video.[114] On 15 April, a Ukrainian Su-25 was reportedly shot down by Russian forces in Izyum.[115] The downing of the aircraft was recorded by a military camera in thermographic mode.[116] The pilot, Captain Yegor Seredyuk, was reported as being killed near Izyum on 15 April.[117][118] Seredyuk was awarded the Hero of Ukraine order.[119] On 14 May a Su-25 from 299th Tactical Aviation Brigade was shot down in Huliaipole, Zaporizhzhia Oblast and the pilot killed.[120][121]

On 14 March 2023, the Minister of Defense of North Macedonia, Slavjanka Petrovska, confirmed the transfer of four non-airworthy Su-25s to Ukraine.[122]

On 2 January 2025, Forbes reported that Ukraine apparently managed to overhaul its remaining Su-25s to carry Western glide bombs such as the French AASM Hammer in 2024, allowing them to operate outside of Russian air defenses range.[123]

Variants

[edit]

Su-25

[edit]
Soviet Su-25 in flight

The basic version of the aircraft was produced at Factory 31, at Tbilisi, in the Soviet Republic of Georgia. Between 1978 and 1989, 582 single-seat Su-25s were produced in Georgia, not including aircraft produced under the Su-25K export program. This variant of the aircraft represents the backbone of the Russian Aerospace Forces' Su-25 fleet, currently the largest in the world.[10] The aircraft experienced a number of accidents in operational service caused by system failures attributed to salvo firing of weapons. In the wake of these incidents, use of its main armament, the 240 mm S-24 rocket, was prohibited. In its place, the FAB-500 500 kg (1,100 lb) general-purpose high-explosive bomb became the primary armament.[10]

Su-25K

[edit]
Czech Republic Su-25K in 1994.

The basic Su-25 model was used as the basis for a commercial export variant, known as the Su-25K (Komercheskiy). This model was also built at Factory 31 in Tbilisi, Georgia. The aircraft differed from the Soviet Air Force version in certain minor details concerning internal equipment. A total of 180 Su-25K aircraft were built between 1984 and 1989.[10]

Su-25UB

[edit]

The Su-25UB trainer (Uchebno-Boyevoy) was drawn up in 1977. The first prototype, called "T-8UB-1", was rolled out in July 1985 and its maiden flight was carried out at the Ulan-Ude factory airfield on 12 August of that year.[10] By the end of 1986, 25 Su-25UBs had been produced at Ulan-Ude before the twin-seater completed its State trials and officially cleared for service with the Soviet Air Force.[124][clarification needed]

It was intended for training and evaluation flights of active-duty pilots, and for training pilot cadets at Soviet Air Force flying schools. The performance did not differ substantially from that of the single-seater. The navigation, attack, sighting devices and weapons-control systems of the two-seater enabled it to be used for both routine training and weapons-training missions.[125]

Su-25UBK

[edit]
Bulgarian Su-25UBK on take-off

From 1986 to 1989, in parallel with the construction of the main Su-25UB combat training variant, the Ulan-Ude plant produced the so-called "commercial" Su-25UBK, intended for export to countries that bought the Su-25K, and with similar modifications to that aircraft.[126]

Su-25UBM

[edit]

The Su-25UBM is a twin seat variant that can be used as an operational trainer, but also has attack capabilities, and can be used for reconnaissance, target designation and airborne control. Its first flight was on 6 December 2008 and it was certified in December 2010. It will enter operational use with the Russian Aerospace Forces later. The variant has a Phazotron NIIR Kopyo radar and Bars-2 equipment on board. Su-25UBM's range is believed to be 1,300 km (810 mi) and it may have protection against infra-red guided missiles (IRGM), a minimal requirement on today's battle fields where IRGMs proliferate.[127]

Su-25UTG

[edit]
Su-25UTG carrier-based trainer aircraft at Novofedorovka airbase

The Su-25UTG (Uchebno-Trenirovochnyy s Gakom) is a variant of the Su-25UB designed to train pilots in takeoff and landing on a land-based simulated carrier deck, with a sloping ski-jump section and arrester wires. The first one flew in September 1988, and approximately 10 were produced.[128] About half remained in Russian service after 1991; they were used on Russia's sole aircraft carrier, Admiral Kuznetsov. This small number of aircraft were insufficient to meet the training needs of Russia's carrier air group, so a number of Su-25UBs were converted into Su-25UTGs. These aircraft being distinguished by the alternative designation Su-25UBP (Uchebno-Boyevoy Palubny)—the adjective palubnyy meaning "deck", indicating that these aircraft have a naval function.[129] As of 2007, approximately 10 of these aircraft were operational in the Russian Navy as part of the 279th Naval Aviation Regiment of the Northern Fleet.[130] In 2021, Su-25 aircraft were also reported deployed with the 100th Independent Shipborne Fighter Aviation Regiment of the same fleet.[131]

Su-25BM

[edit]

The Su-25BM (Buksirovshchik Misheney) is a target-towing variant of the Su-25 whose development began in 1986. The prototype, designated T-8BM1, successfully flew for the first time on 22 March 1990, at Tbilisi. After completion of the test phase, the aircraft was put into production.[129]

The Su-25BM target-tower was designed to provide towed target facilities for training ground forces and naval personnel in ground-to-air or naval surface-to-air missile systems. It is powered by R-195 engines and equipped with an RSDN-10 long-range navigation system, an analogue of the Western LORAN system.[129]

Su-25T

[edit]

The Su-25T (Tankovy) is a dedicated antitank version, which has been combat-tested with notable success in Chechnya.[18] The design of the aircraft is similar to the Su-25UB. The variant was converted to one-seater, with the rear seat replaced by additional avionics.[132] It has all-weather and night attack capability. In addition to the full arsenal of weapons of the standard Su-25, the Su-25T can employ the KAB-500Kr TV-guided bomb and the semi-active laser-guided Kh-25ML.[18] Its enlarged nosecone houses the Shkval optical TV and aiming system with the Prichal laser rangefinder and target designator. It can also carry Vikhr laser-guided, tube-launched missiles, which is its main antitank armament. For night operations, the low-light TV Merkuriy pod system can be carried under the fuselage. Three Su-25Ts prototypes were built in 1983–86 and 8 production aircraft were built in 1990.[133] With the introduction of a definitive Russian Air Force Su-25 upgrade programme, in the form of Stroyevoy Modernizirovannyi, the Su-25T programme was officially canceled in 2000.[134]

Su-25TM (Su-39)

[edit]
Russian Su-25TM has been built in small numbers. Carries (from tip to fuselage) R-73, R-77, 8×Vikhr, Kh-29T, Kh-58. White dome of Kopyo radar container is seen below, while two Omul ECM pods lie beside the aircraft.

A second-generation Su-25T, the Su-25TM (also designated Su-39), has been developed with improved navigation and attack systems, and better survivability. While retaining the built-in Shkval of Su-25T, it may carry Kopyo (rus. "Spear") radar in an under fuselage container, which is used for engaging air targets (with RVV-AE/R-77 missiles) as well as ships (with Kh-31 and Kh-35 antiship missiles). The Russian Air Force has received 8 aircraft as of 2008.[132] Some of the improved avionics systems designed for T and TM variants have been included in the Su-25SM, an interim upgrade of the operational Russian Air Force Su-25, for improved survivability and combat capability.[18] The Su-25TM, as an all-inclusive upgrade programme has been replaced with the "affordable" Su-25SM programme.[134]

Su-25SM

[edit]
A Sukhoi Su-25SM at the Celebration of the 100th anniversary of Russian Air Force

The Su-25SM (Stroyevoy Modernizirovannyi) is an "affordable" upgrade programme for the Su-25, conceived by the Russian Air Force in 2000. The programme stems from the attempted Su-25T and Su-25TM upgrades, which were evaluated and labeled as over-sophisticated and expensive. The SM upgrade incorporates avionics enhancements and airframe refurbishment to extend the Frogfoot's service life by up to 500 flight hours or 5 years.[134]

The Su-25SM's all-new PRnK-25SM "Bars" navigation/attack suite is built around the BTsVM-90 digital computer system, originally planned for the Su-25TM upgrade programme. Navigation and attack precision provided by the new suite is three times better of the baseline Su-25 and is reported to be within 15 m (50 ft) using satellite correction and 200 m (660 ft) without it.[134]

A new KA1-1-01 Head-Up Display (HUD) was added providing, among other things, double the field of view of the original ASP-17BTs-8 electro-optical sight. Other systems and components incorporated during the upgrade include a Multi-Function Display (MFD), RSBN-85 Short Range Aid to Navigation (SHORAN), ARK-35-1 Automatic Direction Finder (ADF), A-737-01 GPS/GLONASS Receiver, Karat-B-25 Flight Data Recorder (FDR), Berkut-1 Video Recording System (VRS), Banker-2 UHF/VHF communication radio, SO-96 Transponder and a L150 "Pastel" Radar Warning Receiver (RWR).[134]

The R-95sh engines have been overhauled and modified with an anti-surge system installed. The system is designed to improve the resistance of the engine to ingested powders and gases during gun and rocket salvo firing.[134]

The combination of reconditioned and new equipment, with increased automation and self-test capability has allowed for a reduction of pre- and post-flight maintenance by some 25 to 30%. Overall weight savings are around 300 kg (660 lb).[134]

Su-25SM weapon suite has been expanded with the addition of the Vympel R-73 highly agile air-to-air missile (albeit without helmet mounted cueing and only the traditional longitudinal seeker mode) and the S-13T 130 mm rockets (carried in five-round B-13 pods) with blast-fragmentation and armour-piercing warheads. Further, the Kh-25ML and Kh-29L Weapon Employment Profiles have been significantly improved, permitting some complex missile launch scenarios to be executed, such as: firing two consecutive missiles on two different targets in a single attack pass. The GSh-30-2 autocannon (250-round magazine) has received three new reduced rate-of-fire modes: 750, 375 and 188 rounds per minute. The Su-25SM was also given new BD3-25 under-wing pylons.[134]

The eventual procurement programme is expected to include between 100 and 130 kits, covering 60 to 70 percent of the Russian Air Force active single-seat fleet, as operated in the early 2000s.[134] On 2012, the Russian Aerospace Forces had over 30 Su-25SMs in service with plans to modernize about 80 Su-25s to the improved standard.[135] By March 2013, over 60 aircraft are to be upgraded.[136] In February 2013, ten new Su-25SMs were delivered to the Air Force southern base,[137][138] where operational training is being conducted.[139] During the period 2005–2015, more than 80 aircraft were upgraded.[140]

Since early 2014, the 368th Assault Aviation Regiment of the 4th Air and Air Defence Forces Army at Budyonnovsk has received advanced Su-25SMs[141] (probably 16 aircraft). Nine more were delivered in 2018,[142][143][144] eight more in early 2019[145][146][147] and four more in early 2020 plus one more in early 2021.[148][149][150]

Since 2018, the Aerospace Forces [VKS] have been receiving Su-25SM3s, and a total of 25 aircraft have already been delivered as of June 2019. Unlike the baseline Su-25 and its incrementally upgraded variant, the Su-25SM, both of which have a rather outdated Klen-PS laser target designator in the nose, the Su-25SM3 has been upgraded with the new SOLT-25 electro-optics nose module. The SOLT-25 provides 16× zoom and features a laser range finder and target designator, thermal imager, TV channels, and the ability to track moving targets in all weather up to 8 km away. In addition, the Su-25SM3 comes with the Vitebsk-25 protection suite, which integrates a set of Zakhvat forward and rearward facing missile approach warning ultraviolet sensors, the L-150-16M Pastel radar homing and warning system, two UV-26M 50 mm chaff dispensers, and a pair of wing-mounted L-370-3S radar jamming pods. Furthermore, the Su-25SM3 has been upgraded with the new PrNK-25SM-1 Bars targeting-and-navigation system and the KSS-25 communication system with Banker-8-TM-1 antenna.[151]

As a result from combat experience in Syria the Su-25SM3 has been equipped with SVP-24 navigation and bombing aids that improve the accuracy of unguided bombs.[152]

Su-25KM

[edit]

The Su-25KM (Komercheski, Modernized),[153] nicknamed "Scorpion", is an Su-25 upgrade programme announced in early 2001 by the original manufacturer, Tbilisi Aircraft Manufacturing in Georgia, in partnership with Elbit Systems of Israel. The prototype aircraft made its maiden flight on 18 April 2001 at Tbilisi in full Georgian Air Force markings.[154] The aircraft uses a standard Su-25 airframe, enhanced with advanced avionics including a glass cockpit, digital map generator, helmet-mounted display, computerised weapons system, complete mission pre-plan capability, and fully redundant backup modes. Performance enhancements include a highly accurate navigation system, pinpoint weapon delivery systems, all-weather and day/night performance, NATO compatibility, state-of-the art safety and survivability features, and advanced onboard debriefing capabilities complying with international requirements.[154] It has the ability to use Israeli Opher infrared-guided bombs and Lizard laser-guided bombs, as well as the Vympel R-73 infrared-guided missile.[155]

Su-28

[edit]
Sukhoi Su-28 non-combat jet trainer

The Sukhoi Su-28 (also designated Su-25UTUchebno-Trenirovochnyy) is an advanced basic jet trainer, built on the basis of the Su-25UB as a private initiative by the Sukhoi Design Bureau. The Su-28 is a light aircraft designed to replace the Czechoslovak Aero L-39 Albatros. Unlike the basic Su-25UB, it lacks a weapons-control system, built-in cannon, weapons hardpoints, and engine armour.[156]

Other

[edit]
  • Su-25R (Razvedchik) – a tactical reconnaissance variant designed in 1978, but never built.[157]
  • Su-25U3 (Uchebnyy 3-myestny) – also known as the "Russian Troika", was a three-seat basic trainer aircraft. The project was suspended in 1991 due to lack of funding.[157]
  • Su-25U (Uchebnyy) – a trainer variant of Su-25s produced in Georgia between 1996 and 1998. Three aircraft were built in total, all for the Georgian Air Force.[157]
  • Su-25M1/Su-25UBM1 – Su-25 and Su-25UB aircraft modernized by the Ukrainian company MiGremont for the Ukrainian Air Force. Ten modernized as of 2013 (seven single-seat and three trainers). Upgrades include a new GPS receiver, a new radio, more accurate weapon delivery thanks to a new sight, and a new digital flight data recorder. Additionally, upgraded aircraft can use S-13 rockets.[158]
  • Ge-31 is an ongoing Georgian program of Tbilisi Aircraft Manufacturing aiming at producing a renewed version of Su-25 without Russian components and parts.[159]
  • T-12 ("Shturmovik-90") – a proposed successor to the Su-25. It would have utilized a twin fuselage with two cockpits; one would carry the pilot, who would also operate the plane's radar, while the other would operate the plane's weapons and fire control. The T-12's design also included a forward-swept wing and V-tail.[160]

Operators

[edit]

Notable accidents

[edit]

The Su-25 has been involved in the following notable aviation accidents.

  • An Su-25K of the Air Force of the Democratic Republic of the Congo disappeared in December 2006 during a routine rebasing operation and no wreckage was ever found.[161]
  • Another Congolese Su-25K crashed on 30 June 2007 during an Independence Day display, near the city of Kisangani, killing the pilot. Investigations revealed that the crash was due to an engine failure.[161]
  • An Su-25 of the Russian Air Force exploded in mid-air on 20 March 2008 during a live firing exercise over the Primorsky Krai, 143 km (89 mi) from Vladivostok, killing the pilot. Further investigations revealed that the aircraft was downed by a missile accidentally launched by a wingman. After the accident, all Russian Su-25s were grounded until the investigation was concluded.[citation needed]

Specifications (Su-25/Su-25K, late production)

[edit]
Legend
  • 1: SPM-17A cannon
  • 2: Air brakes
  • 3: Electronic countermeasures
  • 4: Laser Station Maple-PS
  • 5: Avionics
  • 6: Identification friend or foe system
  • 7: Pitot tube
  • 8: Drogue parachute
  • 9: Fuel tanks
  • 10: Main landing gear
  • 11: K-36L ejection seat
  • 12: Bulletproof glass
  • 13: Periscope
  • 14: Turbojet
  • 15: Air intake
  • 16: RSBN Short Range Navigation System
  • 17: PA-7 Pitot tube
  • 18: Front landing gear
  • 19: Canopy
  • 20: TSA-17 Sight
  • 21: Hinged ladder
  • 22: Longeron
  • 23: Flaps
  • 24: Leading edge slats
  • 25: Empennage, including rudder
  • 26: Aileron
  • 27: ASO-2V infrared countermeasures
  • 28: SPO-15 radar warning receiver
  • 29: Tail flaps
  • 30: CDD-25 hardpoints
  • 31: AAP-60 Starter engines[162]
Sukhoi Su-25 line drawing

Data from Jane's All The World's Aircraft 2003–2004,[163]

General characteristics

  • Crew: 1
  • Length: 15.53 m (50 ft 11 in) (including nose probe)
  • Wingspan: 14.36 m (47 ft 1 in)
  • Height: 4.80 m (15 ft 9 in)
  • Wing area: 33.7 m2 (363 sq ft)
  • Empty weight: 9,800 kg (21,605 lb)
  • Gross weight: 14,600 kg (32,187 lb)
  • Max takeoff weight: 19,300 kg (42,549 lb) [164]
  • Fuel capacity: 3,200 L (850 US gal; 700 imp gal)
  • Powerplant: 2 × Soyuz/Tumansky R-195 turbojet engine, 44.18 kN (9,930 lbf) thrust each

Performance

  • Maximum speed: 975 km/h (606 mph, 526 kn) at sea level
  • Range: 1,000 km (620 mi, 540 nmi) at altitude[164]
  • Combat range: 750 km (470 mi, 400 nmi) at sea level with 4,400 kg (9,700 lb) of ordnance and two external fuel tanks
  • Service ceiling: 7,000 m (23,000 ft)
  • g limits: +6.5
  • Rate of climb: 58 m/s (11,400 ft/min)

Armament

Avionics

See also

[edit]

Related development

Aircraft of comparable role, configuration, and era

References

[edit]
[edit]
Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
The Sukhoi Su-25 (NATO reporting name: Frogfoot) is a single-seat, twin-engine, straight-wing subsonic jet aircraft designed by the Sukhoi Design Bureau for close air support (CAS) roles, emphasizing survivability in low-altitude operations against ground targets. Developed in the Soviet Union during the 1970s to meet a requirement for a dedicated armored attack platform capable of operating near forward lines amid intense anti-aircraft fire, the Su-25 features a robust airframe with extensive pilot protection via a titanium-alloy armored "bathtub" cockpit that withstands hits from small arms and shrapnel up to 23 mm caliber. Powered by two Tumansky R-95Sh turbofan engines providing a maximum speed of approximately 950 km/h and a combat radius of 750 km, it is armed with a twin-barrel 30 mm GSh-30-2 cannon carrying 250 rounds, alongside ten underwing hardpoints for up to 4,400 kg of ordnance including bombs, rockets, and anti-tank missiles. First flown on 22 February 1975 and entering Soviet Air Force service in 1981 after accelerated production starting in 1978, the Su-25 proved its durability in combat during the Soviet–Afghan War, where over 23,000 sorties were flown despite vulnerabilities to man-portable air-defense systems like the Stinger missile, resulting in dozens of losses that informed later upgrades such as improved countermeasures and navigation. Exported to over a dozen nations and produced in more than 1,000 units including variants like the twin-seat trainer Su-25UB and modernized Su-25SM with enhanced avionics, the type remains a cornerstone of Russian tactical airpower and has been employed in conflicts including the Chechen Wars, the 2008 Russo-Georgian War, the Syrian intervention, and the ongoing war in Ukraine, where attrition has highlighted both its resilience and limitations against advanced air defenses.

Development

Origins and Design Requirements

The development of the Sukhoi Su-25 originated in the late 1960s amid Soviet recognition of deficiencies in ground attack capabilities, influenced by lessons from the that demonstrated the effectiveness of rugged, low-speed aircraft like the A-1 Skyraider in roles. Soviet , shaped by anticipated high-intensity in Europe under scenarios, emphasized the need for a dedicated "shturmovik" to revive the World War II-era role of armored attack planes such as the Il-2. In March 1968, the design bureau initiated the T-8 project independently, drawing partial inspiration from the U.S. A-X competition that produced the A-10 Thunderbolt II. A formal competition was launched in March 1969, with Sukhoi's T-8 selected for further development over rival proposals. Design requirements prioritized survivability in contested low-altitude environments over speed or agility, mandating a subsonic twin-engine configuration with engines like the R-95Sh providing approximately 44 kN each. The was required to feature a heavily armored cockpit "tub" up to 25 mm thick, bulletproof , and self-sealing fuel tanks to withstand small-arms and shrapnel damage. Operational specifications included a maximum speed of around 950 km/h, a combat radius of about 750 km, and a payload capacity of up to 4,000 kg across multiple hardpoints, enabling delivery of bombs, rockets, and guided munitions against armored targets. Emphasis was placed on rough-field operations, with high-mounted wings, reinforced , and stability for low-speed maneuvers to support ground forces effectively. A fixed 30 mm GSh-30-2 was integral, offset in the nose to accommodate the armored while providing high-volume fire against tanks and fortifications. These requirements reflected a causal focus on enduring ground fire during frontal missions, distinct from faster strike like the Su-7B it was intended to replace.

Prototyping and Testing

The design bureau initiated construction of the T-8 prototypes following an order on 6 May 1974, with assembly at State Factory 153 in . The static-test airframe, designated T8-0, was delivered on 12 September 1974 for structural evaluations. The first flight-test prototype, T8-1, was completed in November 1974 and delivered to the Zhukovskiy flight test center in December 1974. T8-1 performed its maiden flight on 22 February 1975, piloted by , marking the initial evaluation of the aircraft's basic flight characteristics using RD-9B engines. A second prototype, T8-2, followed with its first flight on 26 December 1975, also equipped with RD-9 engines before being refitted with more powerful R-95Sh turbofans in March 1976 and redesignated T8-2D. Bureau-level flight testing of these prototypes proceeded from 1975 until October 1976, focusing on , stability, and initial systems integration, though progress was hampered by the low priority assigned amid concurrent Su-24 and Su-27 programs. Significant modifications were incorporated during testing, including the upgrade of T8-1 to T8-1D in April 1978, which featured R-95Sh engines, a taller vertical stabilizer, and extended wingtips for improved low-speed handling and engine performance. Issues identified included disorienting effects from wingtip airbrakes during turns, prompting design adjustments. Official state testing commenced in 1978, incorporating combat evaluations in Afghanistan from 16 April to 5 June 1980 using T8-1D and T8-3 prototypes, which logged approximately 100 flights, including 44 tactical missions against insurgent targets. These trials revealed the aircraft's robustness but also resulted in losses: T8-1D crashed in January 1980 with the pilot ejecting safely, and another prototype was destroyed on 23 June 1980, killing the pilot. The combined state and field trials concluded in December 1980, demonstrating the Su-25's effectiveness in roles despite identified weaknesses such as airbrake handling. Approval for series production followed in March 1981, validating the design's survivability and payload capabilities under real combat conditions.

Production and Entry into Service

Production of the baseline Su-25 commenced in 1978 at Factory No. 31 in , within the . This facility manufactured the initial series to fulfill Soviet requirements for a dedicated . The first serial-production Su-25 was delivered to the (VVS) in April 1981, with operations based initially in . By 1989, approximately 582 single-seat Su-25s had been completed at the plant, excluding prototypes and subsequent variants. Overall new-build totals for the type, including two-seat trainers, reached around 1,000 across Soviet and later n facilities, though exact figures vary due to classified production data and post-Soviet disruptions. Manufacturing emphasized ruggedness for frontline operations, with armor plating and reinforced structures integrated from the outset. The Su-25 entered operational service with the VVS on 19 July 1981, marking its acceptance for tactical ground-attack roles. Initial deployments focused on training and evaluation within Soviet assault aviation regiments. Combat debut followed in late 1981 during the Soviet-Afghan War, where Su-25s conducted missions against forces, accumulating thousands of sorties by the conflict's end in 1989. This early use validated the design's survivability in low-altitude, high-threat environments.

Design

Airframe and Structural Features

The Sukhoi Su-25 employs a conventional aerodynamic layout optimized for operations at low altitudes, featuring a shoulder-mounted with a 20-degree sweep on the and straight trailing edges. The wings incorporate construction without external bracing, supporting high maneuverability and short takeoff and landing capabilities on unprepared airstrips. Trapezoidal ailerons are positioned near the wingtips to enhance roll control during low-speed flight. The adopts a , stressed-skin design with an ellipsoidal cross-section, providing structural rigidity while housing fuel tanks, , and armament systems. Its long, slender profile tapers rearward from a rounded nose, integrating air intakes for the engines positioned alongside the fuselage. utilizes a mix of metals for durability and weight balance: approximately 60% aluminum alloys for the primary , 19% for high-stress components, 13.5% for critical armored sections, 2% magnesium alloys, and 5.5% other materials. This composition prioritizes resistance to battle damage over lightweight performance, reflecting the aircraft's role in contested environments. Central to the Su-25's survivability is an armored "" enclosing the and key , constructed from 24 mm thick all-welded alloy plates capable of withstanding small-arms fire and shrapnel. The structure includes a transparent armored windscreen block for forward visibility protection. The tricycle landing gear features retractable single-wheel main legs and a nose leg, reinforced to handle operations from rough fields with minimal runway preparation. Exhaust deflectors positioned rearward of the wing trailing edges reduce and aid in dispersing engine heat away from control surfaces.

Powerplant and Flight Performance

The Sukhoi Su-25 is powered by two non-afterburning twin-spool turbojet engines of the type, each producing 44.1 kN (9,920 lbf) of dry thrust. These engines, manufactured by the , are designed for reliability in forward-area operations, utilizing a modular construction that facilitates field maintenance and repairs under combat conditions. The R-95Sh derives from the series but omits afterburners to minimize infrared signature, reduce fuel consumption at low altitudes, and simplify maintenance in austere environments, prioritizing endurance over supersonic dash capability. Later variants, such as the Su-25SM, incorporate upgraded R-195 engines with marginally higher thrust output of 44.18 kN each, along with improved high-temperature materials for better performance in hot climates. Flight performance emphasizes low-altitude maneuverability and loiter time over high-speed intercepts, with a maximum speed of 975 km/h (Mach 0.82) at . Cruising speed typically ranges from 700 to 850 km/h, optimized for tactical radii of action in roles. The combat radius without external tanks is approximately 495 km on low-level missions, extending to 950 km at higher altitudes, while ferry range with drop tanks exceeds 2,000 km. Service stands at 7,000 m, with an absolute up to 10,000 m, reflecting the aircraft's design focus on operations below 5,000 m to evade and surface-to-air threats. Takeoff and landing distances are 750 m and 600 m respectively on prepared runways, enabling dispersed basing on forward airstrips as short as 800 m. Key performance parameters are summarized as follows:
ParameterValue
Maximum speed ()975 km/h
Cruising speed700–850 km/h
Combat radius (low level)495 km
Ferry range>2,000 km
Service ceiling7,000 m
51 m/s
G-limits+6 / -3 g
These figures derive from baseline Su-25 configurations; upgrades like the Su-25T may alter specifics due to added weight. The engines' at subsonic speeds supports extended sorties, with internal capacity of 3,540 kg enabling up to 2 hours of loiter time at operational altitudes.

Cockpit, Armor, and Survivability Measures

The Su-25's is designed for enhanced pilot protection in contested environments, featuring a low-slung seating position within an all-welded "bathtub" enclosure. This armored structure, composed of plates varying in thickness from 10 mm at the bottom and rear to 24 mm at the front and sides, is engineered to withstand direct impacts from 20-23 mm shells and smaller caliber threats. The armored windscreen and canopy glass provide additional ballistic resistance against 12.7 mm rounds, while a reinforced headrest bulkhead offers further shielding. The 's compact layout prioritizes survivability over comfort, with the pilot accessing the seat via a flip-down and a hinged canopy that opens to the right, though visibility remains limited, particularly to the rear. Survivability extends beyond the cockpit through extensive armor plating on vital systems and redundancy in critical components. armor shields key and control mechanisms, with fire-resistant control rods capable of enduring 12.7 mm bullet strikes. Fuel tanks, totaling 3,600-3,660 liters internally, incorporate self-sealing materials filled with to mitigate puncture damage and explosion risks. The airframe employs damage-resistant load-bearing structures, and engine compartments feature . Twin R-195 engines are mounted with lateral separation under the wings, augmented by a 5 mm firewall and extinguishers to prevent cascading failures from battle damage, a modification informed by losses during the Soviet-Afghan War where 23 Su-25s were downed between 1982 and 1989. Redundant hydraulic flight control systems enable continued operation despite partial failures, contributing to the aircraft's reputation for resilience. Defensive aids include warning receivers, active jammers, and dispensers capable of deploying up to 256 and countermeasures to evade and -guided missiles. These measures, combined with the absence of a rear gunner in favor of structural hardening, reflect a design philosophy emphasizing armor and system duplication over alone, allowing the Su-25 to absorb significant punishment from ground fire during low-altitude missions.

Avionics, Sensors, and Navigation

The Sukhoi Su-25 employs a rugged, simplified architecture designed for in forward areas, prioritizing resistance to electronic warfare and battle damage over advanced computational capabilities. The baseline model lacks an onboard , relying instead on optical and laser-based s to minimize detectable emissions and logistical complexity. This configuration supports day and limited night operations, with instrumentation enabling instrument meteorological condition flights via inertial and radio aids. Central to the targeting suite is the ASP-17BTs-8 electro-optical gunsight, which integrates aiming for the internal cannon and unguided ordnance, augmented by an AKS-750s periscopic camera for low-altitude bombing alignment. The nose-mounted Klyon-PS (also designated Klen-PS) and target designator provides ranging to ground targets at distances up to 10 kilometers under optimal conditions, facilitating employment of laser-homing munitions without external designation. Defensive sensors include the SPO-15 , which detects and classifies emissions across multiple bands to alert the pilot to threats, complemented by optional Gardeniya jammers for active countermeasures. Navigation systems emphasize redundancy and autonomy for low-level penetration. The DISS-7 measures ground speed and drift, while the RSBN short-range navigation aid and RSDN-10 long-range system provide positional updates compatible with Soviet-era ground stations. Additional aids encompass the RV-1S for terrain-following cues, MRP-56P receiver, and ARK-19 , enabling and approach guidance without dependency in the original design. Communication is handled by the R-862 VHF/UHF radio suite, with SRO-2 IFF for identification and SO-69 for air traffic integration. These elements collectively ensure the Su-25's operational persistence in degraded environments, though upgrades in later variants introduce digital enhancements like GPS/ receivers.

Armament and Payload Capabilities

The Sukhoi Su-25 is armed with a fixed twin-barrel GSh-30-2 30 mm located in the lower forward , firing armor-piercing incendiary and high-explosive incendiary rounds at a rate of 3,000 rounds per minute, with a standard ammunition capacity of 250 rounds. This cannon provides against ground targets, including light armor, and is effective at ranges up to 1.8 km. The aircraft features ten underwing hardpoints—five per wing—with the outermost stations rated for lighter loads such as air-to-air missiles and the inner stations capable of heavier ordnance up to 500 kg each. Maximum external payload capacity reaches 4,400 kg, enabling diverse loadouts for missions, though normal combat loads are typically 1,000–2,000 kg to preserve maneuverability and range. configuration prioritizes air-to-ground weapons on central and inner pylons, with outer ones for defensive armament; multiple ejector racks like the MBD-2-67U allow carriage of up to four 100 kg bombs per pylon. Primary air-to-ground munitions include:
  • Unguided rockets: S-5 (57 mm, up to 128 per pod), S-8 (80 mm, up to 20–32 per launcher), S-13 (122 mm), and S-24/S-25 (240–340 mm) for area suppression and anti-armor roles.
  • Bombs: Free-fall general-purpose FAB series (from 100 kg to 500 kg), cluster RBK dispensers, and penetration concrete-piercing bombs, often released in salvos.
  • Guided weapons: Kh-25ML laser-homing missiles for precision strikes against high-value targets, supported by an onboard in later configurations.
Defensive armament consists of R-60 (AA-8 ) infrared-guided missiles on wingtip rails, with provisions for R-73 in upgraded models, enabling engagement of pursuing fighters at short range. Auxiliary options encompass SPPU-22 gun pods (carrying twin GSh-23 23 mm cannons) and UB-32 rocket pods, allowing flexible adaptation to mission requirements while maintaining the aircraft's emphasis on low-altitude, unguided ordnance delivery.

Variants

Baseline and Export Models

The , known by as Frogfoot-A, serves as the baseline single-seat variant designed for operations. It features a rugged with armor protecting the cockpit and critical systems, twin Tumansky R-95Sh non-afterburning engines each providing 44.1 kN of , and a twin-barrel 30 mm GSh-30-2 with 150-250 rounds. The supports up to 4,400 kg of ordnance across ten hardpoints, including bombs, rockets, and guided munitions, with a maximum speed of approximately 950 km/h at low altitude and a combat radius of 650 km. Production commenced at the Aviation Factory (Factory 31) in 1978, with 582 units built by 1989 for Soviet and later n service, excluding export models. The Su-25K represents the primary export model, derived directly from the baseline Su-25 but with simplified to exclude classified Soviet technologies, ensuring compatibility with international customers while maintaining equivalent , powerplant, and armament capabilities. Minor internal equipment adjustments distinguish it from the domestic version, such as reduced integration of advanced targeting systems. Approximately 182 Su-25K aircraft were produced at the same facility between 1984 and 1989. Initial exports included 38 units delivered to the in 1984, followed by sales to nations like , , , and [North Korea](/page/North Korea). Both models emphasize survivability through redundant systems, self-sealing fuel tanks, and countermeasures, with the baseline Su-25 incorporating a nose-mounted for precision strikes. Export Su-25Ks were fully combat-capable, often paired with compatible Western or Soviet-era munitions depending on the recipient's . Production of these core variants ceased in the early following the Soviet Union's dissolution, though the Su-25 design influenced subsequent upgrades.

Trainer and Dual-Control Variants

The Su-25UB, designated as a "training-combat" variant, is a two-seat modification of the baseline Su-25 developed to enable pilot training and tactical practice while retaining operational combat capabilities. Development of the Su-25UB began in 1977 as a dual-control conversion trainer, with prototypes assembled at the Ulan-Ude Aviation Plant in 1985 and the first prototype (T-8U-1) achieving its maiden flight later that year. Approximately 130 to 180 units were produced for the Soviet and later Russian Air Force, featuring a lengthened fuselage to accommodate the rear cockpit for an instructor, dual flight controls, and reduced internal fuel capacity compared to the single-seat model, though external stores and armament options remained similar for realistic combat simulation. The Su-25UBK serves as the export counterpart to the Su-25UB, supplied to foreign operators for purposes with adaptations to meet international standards and compatibility with local weaponry. Around 20 examples were built and delivered to nations including , which operates Su-25UBK aircraft for crew conversion and advanced tactical instruction. These dual-control variants maintain the armored and survivability features of the parent design, ensuring safe exposure to scenarios during instruction. Specialized dual-control derivatives include the Su-25UTG, a naval trainer variant derived from the Su-25UB and optimized for carrier operations with the addition of an arrestor hook, reinforced , and only four underwing hardpoints to reduce weight. A batch of 10 Su-25UTG aircraft was produced specifically to train pilots in takeoff and landing procedures on simulated or actual carrier decks, such as those of the Admiral Kuznetsov. The Su-25UT, an unarmed primary trainer sometimes associated with the Su-28 designation, further extends the lineup by stripping combat systems for basic flight instruction, though production numbers remain limited.

Specialized and Prototype Variants

The initial prototypes of the Su-25, designated T-8 series, included the T-8-1, which achieved first flight on February 22, 1975, powered by Tumansky RD-9B engines, followed by the T-8-2 secondary prototype and the T-8-2D re-engined with R95Sh powerplants to align closer to the production configuration. A static test , T-8-0, supported structural evaluations from 1968, while the T-8-3 served as an additional developmental model. The Su-25T, developed as an anti-tank variant starting in 1981, featured the T8M-1 prototype's first flight on August 17, 1984, with three prototypes constructed (two from Su-25UB conversions and one static test airframe), followed by eight pre-production and up to 22 production units equipped with R-195 engines, the Shkval targeting system, SUV-25T avionics suite, and compatibility for 9M120 Vikhr anti-tank missiles. This configuration emphasized all-weather anti-armor operations with enhanced countermeasures, though full-scale production was limited, and only a few saw combat use in Chechnya. The related Su-25TM (also designated Su-39), a refined multirole evolution of the Su-25T, incorporated provisions for Kopyo radar, R-77 air-to-air missiles, Kh-35 anti-ship weapons, GLONASS/GPS navigation, and towed decoys; three units were built by 1998 but not advanced to series production. Specialized proposals from the 1976-1979 period included the Su-25R tactical variant, equipped for day/night imaging with Su-17-compatible sensor pods but never constructed, and the Su-25V all-weather attack model with the Bars /attack suite. Naval adaptations encompassed preliminary carrier-based designs like the Su-25K ship-attack , featuring folding wings, compatibility, and in-flight refueling for all-weather guided strikes, alongside the Su-25TP for deck operations; none progressed beyond conceptual stages. The Su-25BM target- variant, initiated in 1986 with prototype T-8BM1 first flight on March 22, 1990, integrated a towing winch, R-195 engines, and RSDN-10 , yielding 50 units for anti-aircraft of ground and naval forces while retaining capability. Additional experimental efforts, such as the 1991-proposed Su-25U3 three-seat trainer halted in 1993, aimed at multi-pilot instruction but achieved no production.

Upgrades and Modernizations

Russian Modernization Programs

The Su-25SM modernization program was initiated by the Design Bureau in 2001 to upgrade existing Su-25 aircraft, with the first conversions occurring as early as 1999, focusing on enhancing combat capabilities, navigation accuracy, and ordnance efficiency by 2-3 times while reducing maintenance requirements. Key improvements included the PrNK-25SM navigation system, L-150Pastel , and Klen-PS , replacing the original with an electronic heads-up display (HUD) and (LCD) screen. Engine options were updated to R-95Sh or R-195 variants with better surge margins, and armament enhancements allowed integration of R-73E air-to-air missiles and S-13T rockets, with combat payload increased to 5,000 kg via MBD3-U2T-1 bomb racks; the 30 mm cannon's became variable (1:1 to 1:16). The first six Su-25SM aircraft were delivered to the in December 2006, with over 30 upgraded by 2012 and plans to modernize approximately 80 by 2020, resulting in 1.5 times greater overall combat effectiveness and navigation accuracy of about 15 meters without correction. Building on the Su-25SM, the Su-25SM3 upgrade began in 2013 with through 2014, introducing the Vitebsk-25 electronic warfare suite, navigation for 10-meter accuracy, SVP-24-25 automated sighting system, and encrypted communications extending to 1,000 km range. further evolved with the PrNK-25SM-1 system, MFTsI-0332M , and SOLT-25 electro-optical thermal imaging pod, enabling integration of precision-guided munitions such as and missiles, and guided bombs, and the ability to engage four targets simultaneously compared to two for the SM variant. The SUO-39M armament supported these additions, with initial deliveries of two Su-25SM3 aircraft in December 2015 and three more to the by May 2019; by June 2019, 25 had been delivered overall, with the program accelerating to upgrade a significant portion of the operational fleet, prioritizing districts like the . These incremental modernizations extended the Su-25's service life into the without pursuing a full replacement, emphasizing cost-effective enhancements to roles.

Foreign and Non-Russian Upgrades

The initiated the Su-25M1 modernization program in the early 2000s to extend the operational life and enhance the of its legacy Su-25 fleet, incorporating domestically produced such as systems, a new sighting complex, and digital moving maps for all-weather operations. This upgrade also enabled compatibility with advanced air-to-air missiles like the R-73 and improved targeting accuracy, with the first Su-25M1 and Su-25UBM1 prototypes delivered by late 2011 following work at the MiGremont state enterprise. By the end of 2015, 14 single-seat Su-25M1 variants and 2 dual-control Su-25UBM1 trainers had entered service, at a per-aircraft cost of approximately USD 920,000 in 2012 pricing, excluding major repairs. In Georgia, the Tbilisi Aviation Manufacturing plant, in collaboration with Israel's Elbit Systems, developed the Su-25KM Scorpion upgrade in the early 2000s to address limitations in the original design, focusing on advanced avionics for precision strikes and all-weather capability. The Scorpion featured a redesigned cockpit with enhanced pilot situational awareness, integration of smart munitions, and improved aerodynamics that reportedly tripled operational efficiency compared to baseline models. Approximately 10 aircraft underwent this modification, with the first prototype achieving its maiden flight in 2007, though production efforts stalled amid geopolitical tensions and no further deliveries were confirmed as of 2022. Azerbaijan contracted (TAI) in 2023 for the Laçın upgrade program on its Su-25 fleet, emphasizing integration of Turkish and weaponry to enable stand-off engagements beyond visual range. Key enhancements include Aselsan's Advanced Modular Computer for data processing, multifunction displays, upgraded electronic warfare suites, and compatibility with precision-guided munitions such as gliding bombs, the SOM Sahin (successfully tested in April 2025), and other smart weapons. The program, publicly showcased at ADEX 2024, aims to modernize the aircraft's fire control and navigation systems while preserving its armored role. Bulgaria's outsourced the overhaul and partial upgrade of eight Su-25s (six single-seat Su-25K and two Su-25UBK trainers) to Belarus's 558th Repair Plant in Baranovichi, with work completed between 2020 and 2021 to extend airframe life by 800 flight hours and 10 calendar years. Modifications incorporated new communication radios, GPS/ navigation, a , digital cockpit instruments, and expanded armament options including R-73 missiles, enhancing precision and interoperability with NATO-standard assets. The first returned aircraft landed at Graf Ignatievo on September 21, 2020, with the full batch certified for 40-year total service life post-upgrade.

Operational History

Soviet-Afghan War

The Sukhoi Su-25 entered combat operations in in 1981 as part of the Soviet intervention, with initial deployments from units in Soviet transitioning to active support for ground forces against insurgents. Designed specifically for in rugged terrain, the aircraft operated from forward bases such as and , employing low-altitude tactics to deliver unguided bombs, rockets, and 30 mm cannon fire against troop concentrations, supply convoys, and fortified positions. By the war's end in 1989, nearly 50 Su-25s were based in , forming a core element of Soviet tactical aviation for missions. Throughout the conflict, Su-25 units amassed approximately 60,000 sorties, accounting for a significant portion of fixed-wing ground attack missions that inflicted heavy attrition on forces through repeated strikes on mobile targets and mountain hideouts. The aircraft's titanium-reinforced and double-redundant flight controls enhanced pilot survivability in contested environments, allowing sustained operations despite exposure to small-arms fire and early man-portable air-defense systems (MANPADS). Effectiveness was bolstered by integration with forward air controllers and helicopter gunships, enabling precise coordination for troop extractions and convoy protection, though operational tempo demanded frequent maintenance to counter dust ingestion and battle damage. Attrition proved a persistent challenge, with 23 Su-25s confirmed lost primarily to shoulder-fired missiles and heavy machine guns, representing a loss rate of about 0.038% per sortie—lower than many contemporaries due to the design's emphasis on low-threat evasion and rapid egress. The introduction of U.S.-supplied missiles from 1986 onward increased vulnerabilities, as warhead fragments targeted engine exhausts; a notable cluster of four losses occurred over three days in one engagement, highlighting the need for countermeasures like decoys later retrofitted. Despite these setbacks, the Su-25's ruggedness and capacity—up to 4,400 kg of ordnance—sustained its role until the Soviet withdrawal in February 1989, influencing subsequent doctrinal shifts toward enhanced electronic warfare integration.

Iran-Iraq War and Early Exports

The Iraqi Air Force became an early export customer for the Sukhoi Su-25, acquiring the aircraft during the Iran-Iraq War (1980–1988) to bolster close air support capabilities against Iranian ground forces. Deliveries of the single-seat Su-25K and two-seat Su-25UBK variants commenced in the mid-1980s, enabling Iraq to deploy the Frogfoot in combat operations shortly thereafter. Iraqi Su-25s conducted numerous sorties in support of ground troops, demonstrating the aircraft's ruggedness in a high-threat environment marked by Iranian surface-to-air missiles and anti-aircraft artillery. One notable incident involved an Iraqi Su-25K sustaining a direct hit from an Iranian SAM yet remaining flyable, underscoring its armored design and redundancy features. Losses occurred, including at least one downed by a surface-to-air missile during the conflict. Following initial sales to Iraq, early exports expanded to other nations seeking affordable close air support platforms, though specific details on subsequent deliveries in the late 1980s remain limited in declassified records. Iraq's acquisition marked the Su-25's debut in non-Warsaw Pact service, paving the way for broader proliferation to Middle Eastern and African operators amid Cold War arms dynamics.

Post-Soviet Conflicts in the Caucasus

During the War in Abkhazia from August 1992 to September 1993, the conducted approximately 215 combat sorties with Su-25 aircraft, suffering six losses to ground fire and surface-to-air missiles. Russian Su-25s provided covert support to Abkhaz separatists, with at least one Russian-operated Su-25 downed by Georgian defenses on 20 August 1992 near Gudauta. Abkhaz forces captured and operated captured Georgian Su-25s, including at least two aircraft, enhancing their capabilities against Georgian positions. In the 2008 Russo-Georgian War, triggered by Georgia's offensive into on 7-8 August, Russian Su-25s flew extensive missions, targeting Georgian ground forces in , , and mainland Georgia, including strikes on positions near Gori. The first Russian Su-25 loss occurred over on 8 August to ground fire from South Ossetian militias, followed by additional shootdowns, with the final two confirmed losses on 11 August likely to man-portable air-defense systems. Georgia's Su-25s managed a limited number of sorties despite Russian bombing of their airbases, providing ground support before dispersal to avoid further attrition. Russian losses totaled at least five Su-25s, highlighting vulnerabilities to integrated air defenses in contested airspace. In the Nagorno-Karabakh conflicts, both Armenian and Azerbaijani forces employed Su-25s starting from the First Nagorno-Karabakh War (1988-1994), though detailed sortie data remains sparse. During the Second Nagorno-Karabakh War in September-November 2020, Armenia lost at least two Su-25s: one on 29 September, most likely to an Azerbaijani MiG-29 rather than a claimed Turkish F-16 incursion, and another on 2 November downed by Azerbaijani defenses over the combat zone. Azerbaijan integrated Su-25s into its operations later in the war for low-altitude strikes against Armenian positions, leveraging upgraded variants to support ground advances amid drone-dominated skies. These engagements underscored the Su-25's role in close air support but exposed it to advanced man-portable defenses and electronic warfare, contributing to high attrition rates for fixed-wing assets.

African and Middle Eastern Deployments

The employed Su-25TK and Su-25UBK variants during the (1998–2000), conducting strikes on Eritrean ground targets with capabilities for night-time precision attacks using upgraded electro-optical systems. On 15 May 2000, an Ethiopian Su-25 was shot down by Eritrean anti-aircraft fire during operations near the front lines. In , the has utilized Su-25s in counter-insurgency operations against militants, including cross-border strikes into , the , and since the mid-2010s. Similarly, Côte d'Ivoire's Force Aérienne de Côte d'Ivoire operated four Su-25s during the (2002–2007), employing them for with distinctive sharkmouth . The acquired 15 Su-25s from starting in 2008 and deployed them in against rebel forces, prompting UN concerns over arms embargo violations as observed by envoys in 2010. These aircraft conducted airstrikes in Southern in 2011 using unguided munitions against positions held by the Sudan People's Liberation Movement-North. In the ongoing since 2023, Su-25s based at El Fasher and have targeted supply lines and positions, with Sudanese army reports crediting them for disrupting rebel logistics. In the , the air force deployed two Su-25s in November 2022 for bombing runs against M23 rebel advances in , part of four aircraft acquired in 1999. One Congolese Su-25 was downed by a in January 2023 amid escalated fighting near the Rwandan border. In the , the received surplus Russian Su-25s in June 2014 to bolster operations against forces, integrating them for with rockets and bombs. transferred additional Su-25K and Su-25UBK variants to in 2014 for anti-ISIS strikes, with reports of their use in eastern targeting militant convoys and positions. These deployments emphasized the aircraft's armored survivability in low-altitude attacks against irregular ground threats.

Russian Intervention in Syria

Russia deployed approximately 12 Sukhoi Su-25SM aircraft to Hmeimim Air Base near , , as part of its initial air contingent in late September 2015, shortly after the intervention began on September 30 at the request of Syrian President . These jets, operated by a dedicated squadron from the , were primarily tasked with low-altitude strikes against rebel and Islamist militant positions, often employing unguided "dumb" bombs in the early phases of operations. By early October 2015, Su-25s participated in nearly 100 bombing raids alongside Su-24M and Su-34 aircraft, focusing on targets in support of Syrian ground forces. Throughout the campaign, which intensified through 2016–2018, Su-25SM variants conducted frequent missions, including nighttime operations and coordination with helicopters for up to 70% of certain sorties in contested areas. Russian Su-25s reportedly dropped around 6,000 bombs during the operation, contributing to efforts against groups designated as terrorists by , such as ISIS and various rebel factions. The aircraft's armored design and ability to loiter at low altitudes proved suitable for tactical strikes in rugged terrain, though operations highlighted vulnerabilities to man-portable air-defense systems (MANPADS) prevalent among insurgents. A notable incident occurred on February 3, 2018, when a Russian Su-25SM was shot down by a MANPADS over province in rebel-held territory; the pilot, Major , ejected but was killed in subsequent ground combat after engaging militants with his sidearm. This marked the only confirmed combat loss of a Su-25 during the intervention, underscoring the risks of operating in densely defended despite electronic countermeasures and base proximity. Russian forces maintained Su-25 presence at Hmeimim into later years for ongoing support, with upgrades like improved navigation aiding precision in complex environments, though the platform's reliance on visual targeting limited all-weather efficacy compared to precision-guided munitions platforms.

War in Ukraine

The Russian Aerospace Forces deployed Su-25 aircraft for close air support missions from the outset of the full-scale invasion of Ukraine on February 24, 2022, targeting ground forces and fortifications in contested areas. These operations exposed the aircraft's limitations against dense Ukrainian air defenses, including man-portable systems like Stinger and Igla, anti-aircraft guns, and later first-person-view drones. By mid-2025, open-source analysts had visually confirmed over 40 Russian Su-25 losses, comprising mostly destroyed airframes with a few damaged, representing a substantial attrition rate for the type. Incidents included friendly fire, mid-air collisions with drones, and strikes on power lines during low-level flights, alongside combat shootdowns. Ukrainian forces, operating a pre-war fleet of approximately 43 flyable Su-25s supplemented by donations from allies such as 18 airframes from Macedonia and , sustained at least 20 losses by early 2025, primarily to Russian surface-to-air missiles and fighters early in the conflict. To mitigate vulnerabilities, Ukrainian pilots integrated Western munitions, including French AASM guided bombs, enabling precision strikes from beyond the reach of short-range defenses after depleting Soviet-era rocket stocks. This adaptation improved survivability, with the combination rated as highly effective for targeted attacks on Russian positions. Overall, the conflict demonstrated the Su-25's challenges in a high-threat environment with pervasive short-range air defenses, prompting Russian tactics to shift toward higher-altitude, shorter-duration s that reduced accuracy but preserved airframes. Ukrainian usage emphasized standoff capabilities, contrasting with Russian reliance on traditional low-level close support, which incurred disproportionate losses relative to sortie rates. Independent assessments highlight that while the Su-25 retained utility against mobile targets, its armor offered limited protection against modern infrared-guided missiles and fragmented threats prevalent in .

Combat Performance and Analysis

Strengths in Close Air Support

The Sukhoi Su-25 excels in close air support through its purpose-built design prioritizing survivability in low-altitude, high-threat environments. The aircraft incorporates a heavily armored titanium cockpit enclosure, often described as a "bathtub," with welded sheets up to 24 mm thick to shield the pilot from small-arms fire, shrapnel, and light anti-aircraft rounds. Redundant twin Tumansky R-95Sh turbofan engines enable sustained flight even after damage to one unit, while self-sealing fuel tanks and duplicated hydraulic and control systems further enhance resilience against ground fire. This rugged construction, totaling over 1,100 kg of titanium armor in key areas, allows the Su-25 to absorb hits that would disable less protected platforms, facilitating repeated sorties in contested zones. Its armament configuration supports rapid, high-volume delivery of ordnance against ground targets. The Su-25 carries up to 4,400 kg of across ten external hardpoints, including unguided rockets ranging from 57 mm S-5 to 330 mm S-24, free-fall bombs, and cluster munitions, enabling saturation attacks on troop concentrations, armor, and fortifications. A fixed 30 mm GSh-30-2 with 250 rounds provides and anti-armor capability, effective against light vehicles and at close range. These weapons, combined with a nose-mounted for targeting, allow precise engagement of mobile and stationary threats at the forward edge of battle without reliance on advanced precision-guided munitions. Maneuverability tailored for operations further bolsters its effectiveness. High-aspect-ratio straight wings generate lift for stable low-speed flight below 500 km/h, permitting tight orbits and accurate weapon release in valleys or over rough where higher-performance jets struggle. distances—under 1,000 m on unprepared strips—enable operations from forward bases near the front line, reducing response times to ground requests. This combination of endurance, payload persistence, and tactical flexibility has proven instrumental in suppressing enemy defenses during advances, as evidenced by its sustained use in prolonged conflicts requiring direct .

Vulnerabilities and Attrition Factors

The Su-25's rugged construction, including armored cockpits and redundant systems, provides resilience against small-caliber fire and shrapnel, but its subsonic speed, limited maneuverability, and reliance on low-altitude operations expose it to man-portable air-defense systems (MANPADS) and anti-aircraft in contested environments. The aircraft's twin engines, while durable, emit strong signatures that modern heat-seeking missiles can exploit, and its wings and fuel tanks lack equivalent protection, leading to catastrophic failures upon direct hits. Basic and absence of advanced electronic countermeasures in baseline models further heighten risks against radar-guided threats without prior suppression of enemy air defenses (SEAD). Historical combat data underscores these design limitations. During the Soviet-Afghan War (1979–1989), Soviet Su-25s suffered approximately 23 losses to U.S.-supplied MANPADS, which targeted the aircraft's hot engine exhausts despite countermeasures like flare dispensers introduced later in the conflict. In the 1991 Gulf War, Su-25s proved highly vulnerable to coalition air superiority, with most of the fleet destroyed on the ground or in flight by advanced fighters and precision strikes, as the platform's lack of speed prevented evasion. In the ongoing (2022–present), Russian Su-25 attrition has accelerated due to widespread MANPADS deployment by Ukrainian forces, including Igla and systems, often guided by drone spotting. Open-source visual confirmations document over 40 Russian Su-25 losses, primarily from MANPADS hits during low-level strikes, with additional incidents of from Russian Pantsir systems and mechanical failures amid intensive operations. Ukrainian Su-25s have also faced attrition from Russian ground-based air defenses, though in lower numbers due to more conservative employment. Poor initial pilot training exacerbated losses, as Su-25 crews conducted predictable attack profiles vulnerable to ambushes, while maintenance strains on aging airframes contributed to non-combat crashes, such as wing failures under high-G maneuvers. Key attrition factors include operational tempo exceeding design limits, with pilots flying at altitudes below 50 meters to evade but exposing aircraft to volume fire from and automatic cannons. Dependence on unguided munitions necessitates close passes over targets, amplifying exposure without integrated standoff capabilities in unmodified variants. In high-intensity conflicts, the Su-25's effectiveness diminishes without dedicated SEAD support, leading to sortie rates constrained by loss rates that outpace production and repair capacities for legacy fleets. Upgrades like the Su-25SM add limited warning and precision weapons, but core aerodynamic and signature vulnerabilities persist against proliferated portable defenses.

Comparative Effectiveness

The Sukhoi Su-25 and represent parallel developments in dedicated aircraft, both entering service in the late and optimized for low-altitude operations against ground targets. The Su-25 prioritizes rapid strikes with a top speed of 950 km/h and enhanced maneuverability, enabling quicker evasion of threats like man-portable air-defense systems (MANPADS) compared to the A-10's 706 km/h limit, which favors prolonged over battlefields.
CharacteristicSu-25A-10 Thunderbolt II
Max Speed (km/h)950706
Armor Mass (kg)Up to 1,100 ()~540 ( /pilot)
Payload (kg)4,4007,250
Primary Cannon30 mm GSh-2 (two barrels)30 mm GAU-8 (seven barrels)
Operational Radius (km)~495~1,030
Data reflects baseline models; upgrades vary. The Su-25's smaller size and speed provide advantages in high-threat ingress/egress, with analysts arguing it can counter MANPADS launches from shorter distances due to superior acceleration away from seekers. In contrast, the A-10's heavier armor and redundant /engines—shielded by the horizontal stabilizer from ground fire—enhance post-hit recovery, though its slower profile increases exposure time. Empirical combat data highlights doctrinal differences: the A-10's design suits U.S. air superiority environments, yielding effective CAS in operations like Desert Storm with minimal losses amid suppressed defenses. The Su-25, tested in denser threat zones such as and , has demonstrated ruggedness from austere bases but higher vulnerability to modern MANPADS and short-range SAMs, as evidenced by multiple shootdowns in since 2022. Ukrainian Su-25 operators have adapted by shifting to standoff precision strikes with Western-guided bombs like AASM Hammer, reducing close-exposure risks after exhausting unguided rocket stocks. This evolution underscores the Su-25's flexibility but also its limitations against peer-level integrated air defenses, where neither excels without suppression.

Operators

Current Operators

The Sukhoi Su-25 remains in active service with multiple air forces worldwide as of 2025, primarily for roles in and select export destinations. Operators include , , , , , , , , , , and . Russia maintains the largest fleet, with approximately 132 Su-25 variants active in the despite ongoing attrition from operations in . The Russian Naval Aviation also operates around 10 upgraded Su-25UBM aircraft. continues to deploy a diminished but operational inventory of about 20 Su-25s, adapted for standoff precision strikes amid heavy losses. Belarus fields up to 67 Su-25s as its primary combat aircraft, with plans for local production enhancements. Azerbaijan is modernizing its Su-25 fleet through partnerships, including upgrades by Turkish firms displayed in 2024. Other operators, such as those in Africa and Asia, maintain smaller numbers for regional conflicts, though exact inventories vary due to limited public data and potential maintenance challenges.

Former Operators

The inherited 24 Su-25K single-seat variants and one Su-25UBK tandem-seat trainer from the dissolved in 1993. These aircraft were based primarily at Air Base and used for training and exercises until their retirement in December 2000, after which they were placed in storage at Air Base. Slovakia received 12 Su-25K and one Su-25UBK following the 1993 . The decommissioned its Su-25 fleet in 2002 as part of military modernization efforts ahead of accession, subsequently selling ten aircraft—including nine Su-25Ks and one Su-25UB—to in 2004. The Aerospace Force operated a small number of Su-25s, primarily captured Iraqi examples acquired during the 1991 . These were deployed in support of Iraqi forces against in 2014 before being transferred to , marking the end of IRGC Su-25 operations. The Air Force of Ivory Coast acquired four Su-25s, including two trainers, from Belarus in 2004 for use in the First Ivorian Civil War. The aircraft conducted operations from Air Base until approximately 2006, after which they became non-operational due to maintenance issues and lack of parts, with no evidence of subsequent service.

Specifications

General Characteristics

The Sukhoi Su-25 is a single-seat, twin-engine, subsonic aircraft designed for operations in low-altitude environments with heavy armor protection for the pilot and critical systems. It accommodates one pilot in a titanium "bathtub" armored , emphasizing against ground fire. Key dimensions include a of 15.53 (including pitot probe), a of 14.36 , a height of 4.80 , and a wing area of 30.1 square . The has an empty weight of approximately 9,800 kilograms and a of 17,600 kilograms. It is powered by two non-afterburning Tumansky R-95Sh engines, each delivering 40.2 kN of , later upgradable to R-195 engines with 44.1 kN . Performance specifications encompass a maximum speed of 975 km/h at low altitude, a combat radius of 375 kilometers with typical ordnance loads, a ferry range of 7,500 kilometers with external fuel tanks, and a service ceiling of 10,000 meters. The supports operations from unprepared airstrips up to 1,000 meters in length, with reinforced for rugged field use.
CharacteristicSpecification
Crew1
15.53 m
14.36 m
4.80 m
area30.1
Empty 9,800 kg
Max takeoff 17,600 kg
Powerplant2 × Tumansky R-95Sh turbofans (40.2 kN each)
Max speed (low alt.)975 km/h
Combat radius375 km
Ferry range7,500 km
Service ceiling10,000 m

Armament

The Sukhoi Su-25 is armed with a fixed twin-barrel GSh-30-2 30 mm located in the lower forward , supplied with 250 rounds of and capable of firing at a rate of 3,000 rounds per minute. The cannon provides capability against ground targets, with up to 1.8 km. External armament is carried on ten underwing hardpoints—five per wing—with a maximum warload of 4,000 kg, though normal loads are around 1,340 kg to maintain maneuverability. The outermost pylons are typically reserved for lightweight air-to-air missiles such as the R-60 (NATO: AA-8 Aphid) for self-defense, while inner stations accommodate heavier ordnance including rocket pods, bombs, and guided munitions. Gun pods, such as the SPPU-22 containing twin GSh-23 23 mm cannons with 260 rounds each, can supplement firepower on dedicated pylons. Common unguided stores include rocket pods launching S-5, S-8, S-13, or S-25 series rockets for area suppression, and free-fall bombs like the /500 series or specialized concrete-penetrators. Precision options encompass laser-guided variants such as the Kh-25ML (NATO: AS-10 Karen) or Kh-29L/T (NATO: AS-14 Kedge) air-to-surface missiles for anti-armor and infrastructure strikes, with some upgraded models compatible with Vikhr laser-guided missiles or even Western Mark 82/83 laser-guided bombs. Export variants like the Su-25K have demonstrated integration of additional air-to-air missiles, including the R-73.
Weapon CategorySpecific ExamplesTypical Load per Hardpoint
Air-to-Air MissilesR-60, R-731-2 per outer pylon
Air-to-Surface MissilesKh-25ML, Kh-29L/T1-2 per inner pylon
Rocket PodsS-8 (80 mm), S-13 (122 mm)Pods with 20-32 rockets
Bombs, Up to 500 kg each
Upgraded variants such as the Su-25SM expand compatibility to include anti-radiation missiles like the and enhanced targeting for standoff munitions, improving survivability in contested environments.

Notable Incidents

Combat Losses

During the , Soviet Su-25s flew over 60,000 sorties but sustained 23 losses to anti-aircraft fire, including U.S.-supplied missiles that exploited the aircraft's low-altitude tactics. The initial combat loss occurred on 16 January 1984 near Urgun, when a Strela-2 MANPADS downed the jet. In the Chechen conflicts, Russian Su-25 losses were limited; by November 2000 in the Second Chechen War, at least three had been lost to ground fire and operational factors. A Russian Su-25 was shot down on 3 February 2018 over province in by Syrian rebels using an Igla MANPADS; the pilot ejected safely but was killed in subsequent ground combat. The has inflicted the heaviest toll, with Russia losing nearly 40 Su-25s since February 2022—about one-fifth of its pre-war fleet—primarily to Ukrainian MANPADS and short-range air defenses during missions. has lost 13 Su-25s based on visually confirmed open-source evidence, including 11 destroyed and 2 captured.
ConflictOperatorConfirmed Losses
Soviet–Afghan WarSoviet23
Second Chechen WarRussian3+
Syrian Civil WarRussian1
Russo-Ukrainian WarRussian~40
Russo-Ukrainian WarUkrainian13
These figures underscore the Su-25's vulnerability to infrared-guided missiles in contested environments, despite its armored design and countermeasures.

Non-Combat Accidents

The Sukhoi Su-25 has suffered multiple non-combat accidents since entering service in 1981, with causes frequently involving failures, loss of control, or ground mishaps, though detailed investigations are often limited by military classification. Early Soviet-era losses included a June 23, 1980, crash resulting in one fatality from an unknown cause, and a December 14, 1981, incident with another pilot fatality. On April 26, 1988, a Soviet Su-25 from the 368th Assault Aviation Regiment crashed near Kalyniv Airfield, killing the pilot due to an undetermined factor. Subsequent accidents highlighted recurring technical vulnerabilities. A February 6, 1990, incident at involved no fatalities but led to the aircraft being written off for unknown reasons. On May 21, 2005, a Su-25 crashed into mountains near , , after a port engine fire caused loss of control shortly after takeoff; the pilot ejected safely. In a ground accident on August 7, 2023, a Russian Su-25SM3 (serial 17) was rammed by a truck while being towed at in , rendering it beyond repair with no injuries reported. Operator-specific losses underscore maintenance and training risks. An Su-25UB (3237) crashed on December 4, 2018, during a routine flight near Maralik, killing both pilots; preliminary data indicated loss minutes after takeoff from an airbase, with the cause remaining undetermined. More recently, a Russian Su-25 crashed on March 24, 2025, during a flight in due to dual engine failure, resulting in the deaths of both crew members and no ground injuries. These incidents reflect patterns of mechanical unreliability in high-stress platforms, compounded by operational demands in various air forces.

References

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