Credit
Alexander Mishin · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Su-24MK · Length
Single source22.53 m (73 ft 11 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourceConfiguration
| Specification | Sukhoi Su-24 | TAI TF Kaan |
|---|---|---|
| Type | All-weather tactical bomber / interdictor[source] | Stealth multirole / air superiority fighter[source] |
| National origin | Soviet Union / Russia[source] | Turkey[source] |
| Manufacturer | Sukhoi[source] | Turkish Aerospace Industries[source] |
| Status | In service[source] | Under development |
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-24MK · wings spread
Single source17.64 m (57 ft 10 in) wings spread[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-24MK · Height
Single source6.19 m (20 ft 4 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-24MK · Empty weight
Single sourceGross; Su-24MK · Gross weight
Single sourceMaximum take-off; Su-24MK · Max takeoff weight
Single source22,300 kg (49,163 lb)[source]
38,040 kg (83,864 lb)[source]
43,755 kg (96,463 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-24MK · / M1.6 at high altitude
Single source1,654 km/h (1,028 mph, 893 kn) / M1.6 at high altitude[source]
Ferry; Su-24MK · Ferry range
Single source2,775 km (1,724 mi, 1,498 nmi)[source]
Su-24MK · lo-lo-lo attack mission with 3,000 kg (6,614 lb) of ordnance and external tanks
Single source615 km (382 mi, 332 nmi) lo-lo-lo attack mission with 3,000 kg (6,614 lb) of ordnance and external tanks[source]
Su-24MK · 2 × Lyulka AL-21F-3A turbojet engines thrust each dry
Single sourceSu-24MK · with afterburner
Single source2 × Lyulka AL-21F-3A turbojet engines, 75 kN (17,000 lbf) thrust each dry, 109.8 kN (24,700 lbf) with afterburner[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 sourceSu-24MK · Wing area
Single source55.2 m 2 (594 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-24MK · Service ceiling
Single source11,000 m (36,000 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-24MK · 30,000 ft/min
Single source150 m/s (30,000 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Russian Aerospace Forces Ukrainian Air Force Islamic Republic of Iran Air Force Algerian Air Force[source] | — |
|---|
| Number built | Approximately 1,400[source] | — |
|---|
| Manufactured | 1967–1993[source] | — |
|---|
| Introduction date | 1974[source] | 2030s (planned)[source] |
|---|
| First flight | T-6: 2 July 1967 ( 1967-07-02 ) T-6-2I: 17 January 1970 ( 1970-01-17 )[source] | 21 February 2024[source] |
|---|
| Developed from | Sukhoi S-6[source] | — |
|---|
| Fuel capacity | 11,100 kg (24,471 lb)[source] | — |
|---|
| Guns | 1 × internal 23 mm Gryazev-Shipunov GSh-6-23 M rotary cannon with 500 rounds[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Hardpoints | 9 hardpoints with a capacity of up to 8,000 kg (17,635 lb), with provisions to carry combinations of: Rockets: S-5 S-8 S-13 S-24 B S-25 -OFM/LD Missiles: Air-to-air missiles : 4 × R-60 MK 4 × R-73 E Air-to-surface missiles : 4 × Kh-23 M 4 × Kh-25 ML Kh-59 ME Kh-29 L/T/D Anti-ship missiles : Kh-31 A Anti-radiation missiles : 2 × Kh-28 2 × Kh-58 E Kh-25 MP 2 × Kh-31 P Kh-27 PS Bombs: KAB-500KR TV-guided bomb KAB-500L laser-guided bomb KAB-500OD guided bomb KAB-500S-E satellite-guided bomb KAB-1500KR TV-guided bomb KAB-1500L laser-guided bomb ODAB-500 PM bomb RBK-250 cluster bomb RBK-500 cluster bomb 2 × BETAB-500 bomb[source] | 8 internal; 3 per wing, total 6 external[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Airfoil | TsAGI SR14S-5.376; TsAGI SR16M-10[source] | — |
|---|
| g limits | + 6[source] | +9,0 g & −3,5 g[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Wing loading | 651 kg/m 2 (133 lb/sq ft)[source] | 485 kg/m 2 (99 lb/sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Thrust/weight | 0.6[source] | 0,75[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Rockets | S-5 S-8 S-13 S-24 B S-25 -OFM/LD[source] | — |
|---|
| Missiles | Air-to-air missiles : 4 × R-60 MK 4 × R-73 E Air-to-surface missiles : 4 × Kh-23 M 4 × Kh-25 ML Kh-59 ME Kh-29 L/T/D Anti-ship missiles : Kh-31 A Anti-radiation missiles : 2 × Kh-28 2 × Kh-58 E Kh-25 MP 2 × Kh-31 P Kh-27 PS[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 | KAB-500KR TV-guided bomb KAB-500L laser-guided bomb KAB-500OD guided bomb KAB-500S-E satellite-guided bomb KAB-1500KR TV-guided bomb KAB-1500L laser-guided bomb ODAB-500 PM bomb RBK-250 cluster bomb RBK-500 cluster bomb 2 × BETAB-500 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 name | — | TF or MMU[source] |
|---|
| Designer | — | BAE Systems TAI[source] |
|---|
| Primary user | — | Turkish Air Force[source] |
|---|
| Prototypes | — |
|---|
| Flights | — |
|---|
| Initiated | — | 2010[source] |
|---|
| 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 |
|---|
2 × 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