Credit
Fedor Leukhin · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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At a glance
Measured figures
Su-25/Su-25K, late production · including nose probe
Single source15.53 m (50 ft 11 in) (including nose probe)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Configuration
| Specification | Sukhoi Su-25 | TAI TF Kaan |
|---|---|---|
| Type | Attack aircraft / close air support[source] | Stealth multirole / air superiority fighter[source] |
| National origin | Soviet Union / Russia / Georgia[source] | Turkey[source] |
| Designer | Sukhoi[source] | BAE Systems TAI[source] |
| Built by | TAM Management Tbilisi Aircraft Manufacturing Ulan-Ude Aviation Plant[source] | — |
Preliminary specifications (KAAN development aircraft) · Length
Single source20.3 m (66 ft 7 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
20,3 m (66 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Su-25/Su-25K, late production · Wingspan
Single source14.36 m (47 ft 1 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Wingspan
Single sourcePreliminary specifications (KAAN development aircraft) · Wingspan
Single source13.4 m (44 ft 0 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
13,4 m (44 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Su-25/Su-25K, late production · Height
Single source4.80 m (15 ft 9 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Height
Single sourcePreliminary specifications (KAAN development aircraft) · Height
Single source5 m (16 ft 5 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
5 m (16 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Empty; Su-25/Su-25K, late production · Empty weight
Single sourceGross; Su-25/Su-25K, late production · Gross weight
Single sourceMaximum take-off; Su-25/Su-25K, late production · Max takeoff weight
Single source9,800 kg (21,605 lb)[source]
14,600 kg (32,187 lb)[source]
19,300 kg (42,549 lb)[source]
Maximum take-off; Preliminary specifications (KAAN development aircraft) · Maximum takeoff weight
Single source34,750 kg (76,500 lb)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
34.750 kg (76,500 lb)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Maximum; Su-25/Su-25K, late production · at sea level
Single source975 km/h (606 mph, 526 kn) at sea level[source]
Su-25/Su-25K, late production · at altitude
Single source1,000 km (620 mi, 540 nmi) at altitude[source]
Su-25/Su-25K, late production · at sea level with 4,400 kg (9,700 lb) of ordnance and two external fuel tanks
Single source750 km (470 mi, 400 nmi) at sea level with 4,400 kg (9,700 lb) of ordnance and two external fuel tanks[source]
Su-25/Su-25K, late production · 2 × Soyuz/Tumansky R-195 turbojet engine thrust each
Single source2 × Soyuz/Tumansky R-195 turbojet engine, 44.18 kN (9,930 lbf) thrust each[source]
Preliminary specifications (KAAN development aircraft) · 2 × General Electric F110-GE-129 Turbofan thrust each dry
Single sourcePreliminary specifications (KAAN development aircraft) · with afterburner
Single source2 × General Electric F110-GE-129 Turbofan , 76.3 kN (17.155 lbf) thrust each dry, 131 kN (29,000 lbf) with afterburner[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
2 x 13.150 kgf (2 x 29,000 lb)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Su-25/Su-25K, late production · Wing area
Single source33.7 m 2 (363 sq ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Wing area
Single sourcePreliminary specifications (KAAN development aircraft) · Wing area
Single source71.6 m 2 (770 sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
71,6 m2 (771 ft2)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Su-25/Su-25K, late production · Service ceiling
Single source7,000 m (23,000 ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Service ceiling
Manufacturer claimPreliminary specifications (KAAN development aircraft) · Service ceiling
Single source16,764 m (55,000 ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
16.764 m (55,000 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Su-25/Su-25K, late production · 11,400 ft/min
Single source58 m/s (11,400 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | Under development[source] |
|---|
| Primary users | Russian Aerospace Forces Ukrainian Air Force Korean People's Army Air Force Peruvian Air Force See Operators for others[source] | — |
|---|
| Number built | Over 1,000[source] | — |
|---|
| Manufactured | 1978–2017[source] | — |
|---|
| Introduction date | 19 July 1981[source] | 2030s (planned)[source] |
|---|
| First flight | 22 February 1975 ( 1975-02-22 )[source] | 21 February 2024[source] |
|---|
| Variant | Sukhoi Su-28[source] | — |
|---|
| Fuel capacity | 3,200 L (850 US gal; 700 imp gal)[source] | — |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-2 autocannon with 250 rounds SPPU-22 gun pods for 2 × 23 mm Gryazev-Shipunov GSh-23 autocannons with 260 rounds[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Hardpoints | 11 hardpoints with a capacity of up to 4,000 kg (8,800 lb) of stores, with provisions to carry combinations of: Rockets: UB-16 rocket pods for S-5 rockets UB-32 A rocket pods for S-5 rockets B-8M 1 rocket pods for S-8 rockets S-24 S-25 Missiles: Air-to-air missiles : K-13 A R-60 R-73 E Air-to-surface missiles : Kh-23 Kh-25 ML Kh-29 L 9K121 Vikhr Kh-38 (Su-25SM3) Anti-radiation missiles : Kh-28 Bombs: BETAB-500 concrete-penetrating bomb FAB-250 general-purpose bomb FAB-500 GP bomb FAN-500 bomb KAB-500KR TV-guided bomb ZAB-500 incendiary bomb Other: ASO-2V decoy dispensers (chaff and flare): Su-25s in Syria have been pictured with four rows of ASO-2V decoy dispensers (chaff and flare) along the tailcone's upper surface aft of the vertical stabiliser. Geran-5 drone[source] | 8 internal; 3 per wing, total 6 external[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| 1 | SPM-17A cannon[source] | — |
|---|
| 2 | Air brakes[source] | — |
|---|
| 3 | Electronic countermeasures[source] | — |
|---|
| 4 | Laser Station Maple-PS[source] | — |
|---|
| 5 | Avionics[source] | — |
|---|
| 6 | Identification friend or foe system[source] | — |
|---|
| 7 | Pitot tube[source] | — |
|---|
| 8 | Drogue parachute[source] | — |
|---|
| 9 | Fuel tanks[source] | — |
|---|
| 10 | Main landing gear[source] | — |
|---|
| 11 | K-36L ejection seat[source] | — |
|---|
| 12 | Bulletproof glass[source] | — |
|---|
| 13 | Periscope[source] | — |
|---|
| 14 | Turbojet[source] | — |
|---|
| 15 | Air intake[source] | — |
|---|
| 16 | RSBN Short Range Navigation System[source] | — |
|---|
| 17 | PA-7 Pitot tube[source] | — |
|---|
| 18 | Front landing gear[source] | — |
|---|
| 19 | Canopy[source] | — |
|---|
| 20 | TSA-17 Sight[source] | — |
|---|
| 21 | Hinged ladder[source] | — |
|---|
| 22 | Longeron[source] | — |
|---|
| 23 | Flaps[source] | — |
|---|
| 24 | Leading edge slats[source] | — |
|---|
| 25 | Empennage, including rudder[source] | — |
|---|
| 26 | Aileron[source] | — |
|---|
| 27 | ASO-2V infrared countermeasures[source] | — |
|---|
| 28 | SPO-15 radar warning receiver[source] | — |
|---|
| 29 | Tail flaps[source] | — |
|---|
| 30 | CDD-25 hardpoints[source] | — |
|---|
| 31 | AAP-60 Starter engines[source] | — |
|---|
| g limits | + 6.5[source] | +9,0 g & −3,5 g[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Rockets | UB-16 rocket pods for S-5 rockets UB-32 A rocket pods for S-5 rockets B-8M 1 rocket pods for S-8 rockets S-24 S-25[source] | — |
|---|
| Missiles | Air-to-air missiles : K-13 A R-60 R-73 E Air-to-surface missiles : Kh-23 Kh-25 ML Kh-29 L 9K121 Vikhr Kh-38 (Su-25SM3) Anti-radiation missiles : Kh-28[source] | Air-to-air missiles : GÖKTUĞ missile program: Gökdoğan BVR active radar homing Gökhan ramjet engine powered BVR active radar homing Bozdoğan short-range infrared homing Air-to-surface missiles : SOM Cruise Missile (B1, B2, and J variants) KUZGUN-TJ, Turbojet-powered Air-to-surface missile KUZGUN-KY, Solid fuel Rocket-powered Air-to-surface missile KUZGUN-ER, Turbojet-powered , Air-to-surface missile (According to TUBITAK-SAGE, this missile will be equivalent to Penguin Missiles .) KUZGUN-EW, KUZGUN-EW will be able to carry miniaturised EW payload which will act as a stand-in jammer and suppress enemy air defences to significantly increase the survivability of the aircraft of the Turkish Air Force . AKBABA, Air-to-surface , Anti-radiation Missile (ARM) ROKETSAN ÇAKIR Missile Family , Anti-ship , Air-to-surface , surface-to-surface Cruise Missile .[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Bombs | BETAB-500 concrete-penetrating bomb FAB-250 general-purpose bomb FAB-500 GP bomb FAN-500 bomb KAB-500KR TV-guided bomb ZAB-500 incendiary bomb[source] | Teber-81 ( Mark 81 bomb w/ ROKETSAN Laser Guidance Kit) HGK-82 ( Mark 82 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) KGK-82 ( Mark 82 bomb w/ TUBITAK-SAGE Wing Assisted Guidance Kit) Teber-82 ( Mark 82 bomb w/ ROKETSAN Laser Guidance Kit) HGK-83 ( Mark 83 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) KGK-83 ( Mark 83 bomb w/ TUBITAK-SAGE Wing Assisted Guidance Kit) HGK-84 ( Mark 84 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) LHGK-84 ( Mark 84 bomb w/ TUBITAK-SAGE Laser Sensitive Guidance Kit) SARB-83, Bunker buster NEB-84, Bunker buster MAM (Smart Micro Munition) (MAM-T variant) KUZGUN-SS, Glide bomb ASELSAN Miniature Bomb[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Other | ASO-2V decoy dispensers (chaff and flare): Su-25s in Syria have been pictured with four rows of ASO-2V decoy dispensers (chaff and flare) along the tailcone's upper surface aft of the vertical stabiliser. Geran-5 drone[source] | — |
|---|
| Manufacturer | Sukhoi, Tbilisi Aircraft Manufacturing, Ulan-Ude Aviation Plant[source] | Turkish Aerospace Industries[source] |
|---|
| Other name | — | TF or MMU[source] |
|---|
| Primary user | — | Turkish Air Force[source] |
|---|
| Prototypes | — |
|---|
| Flights | — |
|---|
| Initiated | — | 2010[source] |
|---|
| Wing loading | — | 485 kg/m 2 (99 lb/sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Thrust/weight | — | 0,75[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated RF System (IRFS) | — | MURAD-600A AESA radar Radar warning receiver[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated Electro-Optical System (IEOS) | — | KARAT-200 Infrared Search and Track (IRST) TOYGUN Electro-optical reconnaissance, surveillance and targeting system İRİS-300 Missile approach warning system (IR-MWS/360° day/night imaging) YILDIRIM-300 Directional Infrared Counter Measures (DIRCM) LİAS-300 Laser warning receiver (LWS)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated Communications Navigation and IFF (ICNI) | — | ICNAir-ASQ9683 communications suite ARVEN radio-navigation equipment IdentIFF Mode-5 identification friend or foe[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Advanced Cockpit / Human Machine Interface | — | TULGAR Helmet-mounted display (HMDS) LAD-208 Large area display (LAD)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Positive / Negative G Limit | — | +9 / -3,5 G[source]KAAN development aircraft; manufacturer technical data, configuration not stated |
|---|