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At a glance
Measured figures
Su-27PU/Su-30 · Length
Single source21.935 m (72 ft 0 in)[source]
Su-35S · Length
Single sourceConfiguration
| Specification | Sukhoi Su-30 | Sukhoi Su-35 |
|---|---|---|
| Type | Multirole fighter[source] | Multirole fighter[source] |
| National origin | Soviet Union Russia[source] | Soviet Union ( Russia since 1991)[source] |
| Designer | Sukhoi[source] | Sukhoi Design Bureau[source] |
| Built by | KnAAPO Irkut Corporation Hindustan Aeronautics Limited (built by HAL in India under license)[source] | Sukhoi |
21.9 m (71 ft 10 in)[source]
Empty; Su-27PU/Su-30 · Empty weight
Single sourceGross; Su-27PU/Su-30 · Gross weight
Single sourceMaximum take-off; Su-27PU/Su-30 · Max takeoff weight
Single source17,700 kg (39,022 lb)[source]
24,900 kg (54,895 lb)[source]
34,500 kg (76,059 lb)[source]
Empty; Su-35S · Empty weight
Single sourceGross; Su-35S · with 50% internal fuel
Single sourceMaximum; Su-27PU/Su-30 · at high altitude
Single source2,120 km/h (1,320 mph, 1,140 kn) at high altitude[source]
Su-27PU/Su-30 · at high altitude
Single source3,000 km (1,900 mi, 1,600 nmi) at high altitude[source]
Su-35S · approx
Single source1,600 km (990 mi, 860 nmi) approx[source]
Su-27PU/Su-30 · 2 × Saturn AL-31FL /FP Afterburning turbofan engines thrust each dry
Single sourceSu-27PU/Su-30 · with afterburner
Single source2 × Saturn AL-31FL /FP Afterburning turbofan engines, 74.5 kN (16,700 lbf) thrust each dry, 122.58 kN (27,560 lbf) with afterburner[source]
Su-35S · 2 × Saturn AL-41F1S afterburning turbofan engines thrust each dry
Single sourceSu-35S · in emergency power
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In service[source] |
|---|
| Primary users | Russian Aerospace Forces Indian Air Force People's Liberation Army Air Force Algerian Air Force[source] | Russian Aerospace Forces People's Liberation Army Air Force Algerian Air Force[source] |
|---|
| Number built | 630+ (as of 2019 )[source] | Su-27M: 12 Su-35S: 155+[source] |
|---|
| Manufactured | 1992–present[source] | Su-27M: 1987–1995 Su-35S: 2007–present[source] |
|---|
| Introduction date | 1992 (Su-30) 2013 (Su-30SM)[source] | February 2014[source] |
|---|
| First flight | 31 December 1989 ( 1989-12-31 )[source] | Su-27M: 28 June 1988 ( 1988-06-28 ) Su-35S: 19 February 2008 ( 2008-02-19 )[source] |
|---|
| Developed from | Sukhoi Su-27[source] | Sukhoi Su-27[source] |
|---|
| Variants | Sukhoi Su-30MKI Sukhoi Su-30MKK Sukhoi Su-30MKM Sukhoi Su-30MKA[source] | — |
|---|
| Fuel capacity | 9,400 kg (20,723 lb) internal[source] | 11,500 kg (25,400 lb) internal[source] |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] | 1 × internal 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Hardpoints | 12 hardpoints with a capacity of up to 8,000 kg (18,000 lb), with provisions to carry combinations of: Rockets: S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU Missiles: Air-to-air missiles : R-27 R/ER/T/ET/P/EA R-73 E/M RVV-AE (R-77)-1/M R-37M (on the SM2 variant) Air-to-surface missiles : Kh-29 TE/L Kh-59 M/ME Anti-ship missiles : Kh-31 A Anti-radiation missiles : Kh-31 P Bombs: KAB-500KR general-purpose bomb KAB-500OD bomb KAB-1500KR GP bomb KAB-1500L laser-guided bomb FAB-500T GP bomb BETAB-500 SHP bomb ODAB-500PM bomb OFAB-250-270 bomb OFAB-100-120 bomb P-50T bomb RBK-500 cluster bombs SPBE-D bomb[source] | 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] |
|---|
| g limits | + 9[source] | + 9[source] |
|---|
| Wing loading | 401 kg/m 2 (82 lb/sq ft) with 56% fuel[source] | 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] |
|---|
| Thrust/weight | 1 with 56% fuel[source] | 1.13 with 50% fuel 0.92 with full internal fuel[source] |
|---|
| Rockets | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] | S-25 air-ground rocket S-13 air-ground rocket[source] |
|---|
| Missiles | Air-to-air missiles : R-27 R/ER/T/ET/P/EA R-73 E/M RVV-AE (R-77)-1/M R-37M (on the SM2 variant) Air-to-surface missiles : Kh-29 TE/L Kh-59 M/ME Anti-ship missiles : Kh-31 A Anti-radiation missiles : Kh-31 P[source] | 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] |
|---|
| Bombs | KAB-500KR general-purpose bomb KAB-500OD bomb KAB-1500KR GP bomb KAB-1500L laser-guided bomb FAB-500T GP bomb BETAB-500 SHP bomb ODAB-500PM bomb OFAB-250-270 bomb OFAB-100-120 bomb P-50T bomb RBK-500 cluster bombs SPBE-D bomb[source] | 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] |
|---|
| Manufacturer | Sukhoi, Komsomolsk-on-Amur Aircraft Production Association, Yakovlev Corporation[source] | United Aircraft Corporation (for Su-35S)[source] |
|---|
| Variant | — | Sukhoi Su-37[source] |
|---|
| Airfoil | — | 5%[source] |
|---|
Maximum 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]
Su-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]