Credit
Anna Zvereva from Tallinn, Estonia · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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At a glance
Measured figures
Su-35S · Length
Single source21.9 m (71 ft 10 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourceConfiguration
| Specification | Sukhoi Su-35 | TAI TF Kaan |
|---|---|---|
| Type | Multirole fighter[source] | Stealth multirole / air superiority fighter[source] |
| National origin | Soviet Union ( Russia since 1991)[source] | Turkey[source] |
| Manufacturer | United Aircraft Corporation (for Su-35S)[source] | Turkish Aerospace Industries[source] |
| Designer | Sukhoi Design Bureau[source] | BAE Systems TAI |
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-35S · Wingspan
Single source15.3 m (50 ft 2 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-35S · Height
Single source5.9 m (19 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-35S · Empty weight
Single sourceGross; Su-35S · with 50% internal fuel
Single sourceMaximum take-off; Su-35S · Max takeoff weight
Single source19,000 kg (41,888 lb)[source]
25,300 kg (55,777 lb) with 50% internal fuel[source]
34,500 kg (76,059 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
Su-35S · approx
Single source1,600 km (990 mi, 860 nmi) approx[source]
Su-35S · 2 × Saturn AL-41F1S afterburning turbofan engines thrust each dry
Single sourceSu-35S · in emergency power
Single sourceSu-35S · with afterburner
Single source2 × Saturn AL-41F1S afterburning turbofan engines, 86.3 kN (19,400 lbf) thrust each dry, 137.3 kN (30,900 lbf) with afterburner, 142.2 kN (32,000 lbf) in emergency power[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-35S · Wing area
Single source62 m 2 (670 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-35S · Service ceiling
Single source18,000 m (59,000 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-35S · (55,000 ft/min) +
Single source280 m/s (55,000 ft/min) +[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Built by | Sukhoi[source] | — |
|---|
| Status | In service[source] | Under development[source] |
|---|
| Primary users | Russian Aerospace Forces People's Liberation Army Air Force Algerian Air Force[source] | — |
|---|
| Number built | Su-27M: 12 Su-35S: 155+[source] | — |
|---|
| Manufactured | Su-27M: 1987–1995 Su-35S: 2007–present[source] | — |
|---|
| Introduction date | February 2014[source] | 2030s (planned)[source] |
|---|
| First flight | Su-27M: 28 June 1988 ( 1988-06-28 ) Su-35S: 19 February 2008 ( 2008-02-19 )[source] | 21 February 2024[source] |
|---|
| Developed from | Sukhoi Su-27[source] | — |
|---|
| Variant | Sukhoi Su-37[source] | — |
|---|
| Fuel capacity | 11,500 kg (25,400 lb) internal[source] | — |
|---|
| Guns | 1 × internal 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Hardpoints | 12 hardpoints, consisting of 2 wingtip rails, and 10 wing and fuselage stations with a capacity of 8,000 kg (17,630 lb) of ordnance , with provisions to carry combinations of: Rockets: S-25 air-ground rocket S-13 air-ground rocket Missiles: Air-to-air missiles : 8 × R-27 ER/ET 6 × R-73 E/M 12 × R-77 M/P/T/-1 6 × R-74 2 x R-37 Air-to-surface missiles : 6 × Kh-29 L/TE 3 × 3M-14AE Anti-ship missiles : 3 × 3M-54AE1 6 × Kh-31 A/AD Kh-35 U 5 × Kh-59 MK 1 × P-800 Oniks Anti-radiation missiles : 6 × Kh-31 P/PD 5 × Kh-58 UShE Bombs: 8 × KAB-500KR TV-guided bombs 8 × KAB-500L laser-guided bombs 8 × KAB-500OD guided bombs 8 × KAB-500S-E satellite-guided bombs 3 × KAB-1500KR TV-guided bombs 3 × KAB-1500L laser-guided bombs[source] | 8 internal; 3 per wing, total 6 external[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 |
|---|
| Wing loading | 408 kg/m 2 (84 lb/sq ft) With 50% fuel 500.8 kg/m 2 (102.6 lb/sq ft) with full internal fuel[source] | 485 kg/m 2 (99 lb/sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Thrust/weight | 1.13 with 50% fuel 0.92 with full internal fuel[source] | 0,75[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Rockets | S-25 air-ground rocket S-13 air-ground rocket[source] | — |
|---|
| Missiles | Air-to-air missiles : 8 × R-27 ER/ET 6 × R-73 E/M 12 × R-77 M/P/T/-1 6 × R-74 2 x R-37 Air-to-surface missiles : 6 × Kh-29 L/TE 3 × 3M-14AE Anti-ship missiles : 3 × 3M-54AE1 6 × Kh-31 A/AD Kh-35 U 5 × Kh-59 MK 1 × P-800 Oniks Anti-radiation missiles : 6 × Kh-31 P/PD 5 × Kh-58 UShE[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 | 8 × KAB-500KR TV-guided bombs 8 × KAB-500L laser-guided bombs 8 × KAB-500OD guided bombs 8 × KAB-500S-E satellite-guided bombs 3 × KAB-1500KR TV-guided bombs 3 × KAB-1500L laser-guided 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 |
|---|
| Other name | — | TF or MMU[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