Credit
Vitaly V. Kuzmin · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
Su-34 · Length
Single source23.34 m (76 ft 7 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourceConfiguration
| Specification | Sukhoi Su-34 | TAI TF Kaan |
|---|---|---|
| Type | Fighter-bomber / strike fighter[source] | Stealth multirole / air superiority fighter[source] |
| National origin | Soviet Union / Russia[source] | Turkey[source] |
| Manufacturer | Sukhoi , Novosibirsk Aircraft Production Association (NAPO)[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-34 · Wingspan
Single source14.7 m (48 ft 3 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-34 · Height
Single source6.09 m (20 ft 0 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-34 · Empty weight
Single sourceGross; Su-34 · Gross weight
Single sourceMaximum take-off; Su-34 · Max takeoff weight
Single source22,500 kg (49,604 lb)[source]
39,000 kg (85,980 lb)[source]
45,100 kg (99,428 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
Ferry; Su-34 · Ferry range
Single source4,500 km (2,800 mi, 2,400 nmi)[source]
Su-34 · radius of action with standard 12,000 kg weapons load
Single source1,100 km (680 mi, 590 nmi) (radius of action with standard 12,000 kg weapons load)[source]
Su-34 · 2 × Saturn AL-31FM1 afterburning turbofan engines with afterburner
Single source2 × Saturn AL-31FM1 afterburning turbofan engines, 132 kN (30,000 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 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-34 · Wing area
Single source62.04 m 2 (667.8 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-34 · Service ceiling
Single source17,000 m (56,000 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
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Russian Aerospace Forces Algerian Air Force[source] | — |
|---|
| Number built | >163 (7 test and 156 serial aircraft in early 2024)[source] | — |
|---|
| Manufactured | 2006–present[source] | — |
|---|
| Introduction date | 20 March 2014[source] | 2030s (planned)[source] |
|---|
| First flight | 13 April 1990 ( 1990-04-13 )[source] | 21 February 2024[source] |
|---|
| Developed from | Sukhoi Su-27[source] | — |
|---|
| Fuel capacity | 12,100 kg (26,676 lb) internals[source] | — |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 180 rounds[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Airfoil | 5%[source] | — |
|---|
| g limits | + 9[source] | +9,0 g & −3,5 g[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 : R-27 R/ER/T/ET R-73 R-77 Air-to-surface missiles : Kh-25 ML/MT Kh-29 L/T/D Kh-31 A/AD Kh-35 U Kh-38 MAE/MKE/MLE/MTE Kh-58 Kh-59 ME/MK/MK2 Kh-47M2 Anti-ship missiles : P-800 Oniks weight of 1500 kg with a range of up to 300 km and a speed in the range of numbers Mach 2.2–3.0. Officially not in service. Kh-41 Anti-radiation missiles : Kh-25 MP Kh-58 Kh-31 P/PD Cruise missiles : Kh-36 Grom-E1 Kh-65 S/SE Kh-SD[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 OFAB-250-270 bomb OFAB-100-120 bomb FAB-500T general-purpose bomb FAB-250 UMPK gliding bomb FAB-500 UMPK gliding bomb FAB-1500 UMPK gliding bomb FAB-3000 UMPK gliding bomb 2 × BETAB-500 SHP P-50T bomb ODAB-500PM bomb RBK-500 cluster bomb SPBE-D bomb UMPB D-30SN glide 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 |
|---|
| Hardpoints | 12 × on wing and fuselage with a capacity of 12,000–14,000 kilograms (26,000–31,000 lb)[source] | 8 internal; 3 per wing, total 6 external[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] |
|---|
| Wing loading | — | 485 kg/m 2 (99 lb/sq ft)[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 |
|---|