Credit
Alex Beltyukov · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Su-27PU/Su-30 · Length
Single source21.935 m (72 ft 0 in)[source]
Su-57E · Length
Single sourceConfiguration
| Specification | Sukhoi Su-30 | Sukhoi Su-57 |
|---|---|---|
| Type | Multirole fighter[source] | Stealth multirole fighter[source] |
| National origin | Soviet Union Russia[source] | Russia[source] |
| Designer | Sukhoi[source] | Sukhoi[source] |
| Built by | KnAAPO Irkut Corporation Hindustan Aeronautics Limited (built by HAL in India under license)[source] | Komsomolsk-on-Amur Aircraft Plant |
20.1 m (65 ft 11 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-57E · Empty weight
Single sourceGross; Su-57E · at full load
Single sourceMaximum; Su-27PU/Su-30 · at high altitude
Single source2,120 km/h (1,320 mph, 1,140 kn) at high altitude[source]
Maximum; Su-57E · at sea level
Single sourceMaximum; Su-57E · Mach 2.0 at high altitude Mach 1.1
Single sourceMach 2.0, 2,135 km/h (1,153 kn; 1,327 mph) at high altitude Mach 1.1, 1,350 km/h (729 kn; 839 mph) at sea level[source]
Su-27PU/Su-30 · at high altitude
Single source3,000 km (1,900 mi, 1,600 nmi) at high altitude[source]
Su-57E · Combat range
Single source1,250 km (780 mi, 670 nmi)[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-57E · 2 × Saturn AL-41F-1 afterburning turbofan thrust each dry
Single sourceSu-57E · in emergency power
Single sourceSu-27PU/Su-30 · 45,000 ft/min
Single source230 m/s (45,000 ft/min)[source]
Su-57E · Hardpoints: 12 hardpoints (6 × internal, 6 × external) with a capacity of maximum payload
Single sourceHardpoints: 12 hardpoints (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | In service[source] | In production[source] |
|---|
| Primary users | Russian Aerospace Forces Indian Air Force People's Liberation Army Air Force Algerian Air Force[source] | Russian Aerospace Forces Algerian Air Force[source] |
|---|
| Number built | 630+ (as of 2019 )[source] | 44+ as of 2026 (including 10 test aircraft)[source] |
|---|
| Manufactured | 1992–present[source] | 2019–present[source] |
|---|
| Introduction date | 1992 (Su-30) 2013 (Su-30SM)[source] | 2020[source] |
|---|
| First flight | 31 December 1989 ( 1989-12-31 )[source] | 29 January 2010 ( 2010-01-29 )[source] |
|---|
| Developed from | 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] | 9,700 kg (21,385 lb) internal, 12,900 kg (28,440 lb) with 2× PTB-2000 2,000 L (528 US gal) drop tanks[source] |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon[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 (6 × internal, 6 × external) with a capacity of 7,500 kilograms (16,500 lb) maximum payload[source] |
|---|
| g limits | + 9[source] | +9.0[source] |
|---|
| Wing loading | 401 kg/m 2 (82 lb/sq ft) with 56% fuel[source] | 371 kg/m 2 (76 lb/sq ft) normal takeoff weight[source] |
|---|
| Thrust/weight | 1 with 56% fuel[source] | 1.09 at normal takeoff weight (0.97 at loaded weight with full fuel)[source] |
|---|
| Rockets | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[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 : R-77 M R-74M2 R-37 (missile) Air-to-surface missiles : 4 × Kh-38 M 4 × Kh-69 S-71K Kovyor Anti-ship missiles : 2 × Kh-35 U 2 × Kh-31 Anti-radiation missiles : 4 × Kh-58 UShK[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] | KAB-250 guided bomb KAB-500 guided bomb "Drill" anti-tank 500 kg cluster bomb with active homing[source] |
|---|
| Manufacturer | Sukhoi, Komsomolsk-on-Amur Aircraft Production Association, Yakovlev Corporation[source] | United Aircraft Corporation[source] |
|---|
| Variant | — | Sukhoi/HAL FGFA (cancelled)[source] |
|---|
| Supercruise | — | Mach 1.3, 1,400 km/h (756 kn; 870 mph) supercruise at high altitude[source] |
|---|
Gross; Su-57E · normal takeoff weight
Single sourceMaximum take-off; Su-57E · Max takeoff weight
Single source18,500 kg (40,786 lb)[source]
26,700 kg (58,863 lb) normal takeoff weight, 29,800 kg (65,700 lb) at full load[source]
34,000 kg (74,957 lb)[source]
Su-57E · with afterburner
Single source2 × Saturn AL-41F-1 afterburning turbofan , 88.3 kN (19,900 lbf) thrust each dry, 142.2 kN (32,000 lbf) with afterburner, 147.1 kN (33,100 lbf) in emergency power[source]