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Hoangprs5 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
Su-17M4 · Length
Single source19.02 m (62 ft 5 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourceConfiguration
| Specification | Sukhoi Su-17 | TAI TF Kaan |
|---|---|---|
| Type | Fighter-bomber[source] | Stealth multirole / air superiority fighter[source] |
| National origin | Soviet Union[source] | Turkey[source] |
| Manufacturer | Sukhoi[source] | Turkish Aerospace Industries[source] |
| Status | In limited 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-17M4 · wings spread
Single source13.68 m (44 ft 11 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-17M4 · Height
Single source5.12 m (16 ft 10 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-17M4 · Empty weight
Single sourceGross; Su-17M4 · Gross weight
Single sourceMaximum take-off; Su-17M4 · Max takeoff weight
Single source12,160 kg (26,808 lb)[source]
16,400 kg (36,156 lb)[source]
19,430 kg (42,836 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-17M4 · / M1.13 at sea level
Single source1,400 km/h (870 mph, 760 kn) / M1.13 at sea level[source]
Ferry; Su-17M4 · Ferry range
Single source2,300 km (1,400 mi, 1,200 nmi)[source]
Su-17M4 · hi-lo-hi attack with 2,000 kg (4,409 lb) warload
Single source1,150 km (710 mi, 620 nmi) hi-lo-hi attack with 2,000 kg (4,409 lb) warload[source]
Su-17M4 · 1 × Lyulka AL-21F-3 afterburning turbojet engine thrust dry
Single sourceSu-17M4 · with afterburner
Single source1 × Lyulka AL-21F-3 afterburning turbojet engine, 76.4 kN (17,200 lbf) thrust 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-17M4 · wings spread
Single source38.5 m 2 (414 sq ft) wings spread[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-17M4 · Service ceiling
Single source14,200 m (46,600 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-17M4 · 45,000 ft/min
Single source230 m/s (45,000 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Soviet Air Forces (historical) Syrian Air Force (historical) Polish Air Force (historical) Vietnam People's Air Force Islamic Revolutionary Guard Corps[source] | — |
|---|
| Number built | 2,867[source] | — |
|---|
| Manufactured | 1969–1990[source] | — |
|---|
| Introduction date | 1970[source] | 2030s (planned)[source] |
|---|
| First flight | 2 August 1966[source] | 21 February 2024[source] |
|---|
| Developed from | Sukhoi Su-7[source] | — |
|---|
| Fuel capacity | 3,770 kg (8,311 lb)[source] | — |
|---|
| Guns | **2 × 30 mm Nudelman-Rikhter NR-30 autocannons (80 rounds per gun, 160 rounds total) UPK-23 or SPPU-22 gun pods for 2 × Gryazev-Shipunov GSh-23 L autocannons[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Hardpoints | 10 hardpoints with a capacity of up to 4,000 kg (8,800 lb) of stores, with provisions to carry combinations of: Missiles: *** Air-to-air missiles : K-13 R-60 R-73 Air-to-surface missiles : Kh-23 Grom Kh-25 ML Kh-29 L/T/D Anti-radiation missiles : Kh-58 Kh-27 PS Kh-28 Bombs: drop bombs, laser-guided bombs , electro-optical bombs, napalm bombs, drag chute bombs and cluster bombs[source] | 8 internal; 3 per wing, total 6 external[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Airfoil | root: TsAGI SR-3S (5.9%); tip: TsAGI SR-3S (4.7%)[source] | — |
|---|
| g limits | + 7[source] | +9,0 g & −3,5 g[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Wing loading | 443 kg/m 2 (91 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 | 0.68[source] | 0,75[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Missiles | *** Air-to-air missiles : K-13 R-60 R-73 Air-to-surface missiles : Kh-23 Grom Kh-25 ML Kh-29 L/T/D Anti-radiation missiles : Kh-58 Kh-27 PS 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 | drop bombs, laser-guided bombs , electro-optical bombs, napalm bombs, drag chute bombs and cluster bombs[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 |
|---|
| Rockets | S-5 , S-8 & S-13[source] | — |
|---|
| 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