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At a glance
Measured figures
J-10C · Length
Single source16.9 m (55 ft 5 in)[source]
Su-27PU/Su-30 · Length
Single sourceConfiguration
| Specification | Chengdu J-10 | Sukhoi Su-30 |
|---|---|---|
| Type | Multirole combat aircraft[source] | Multirole fighter[source] |
| National origin | China[source] | Soviet Union Russia[source] |
| Manufacturer | Chengdu Aircraft Corporation (1996 - 2024) Guizhou Aircraft Corporation (2024 - present)[source] | Sukhoi, Komsomolsk-on-Amur Aircraft Production Association, Yakovlev Corporation[source] |
| Designer | Chengdu Aircraft Design Institute[source] |
21.935 m (72 ft 0 in)[source]
Gross; J-10C · Gross weight
Single source14,000 kg (30,865 lb)[source]
J-10C · Combat range
Single source1,240 km (770 mi, 670 nmi)[source]
J-10C · 1 × WS-10 B afterburning turbofan engines thrust
Single sourceJ-10C · with afterburner
Single source1 × WS-10 B afterburning turbofan engines, 89.17 kN (20,050 lbf) thrust , 135 kN - 144 kN with afterburner[source]
Su-27PU/Su-30 · 2 × Saturn AL-31FL /FP Afterburning turbofan engines thrust each dry
Single sourceSu-27PU/Su-30 · with afterburner
Single sourceSu-27PU/Su-30 · Service ceiling
Single source17,300 m (56,800 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Sukhoi[source]
| Status | In service[source] | In service[source] |
|---|
| Primary users | People's Liberation Army Air Force Pakistan Air Force Uzbekistan Air and Air Defence Forces[source] | Russian Aerospace Forces Indian Air Force People's Liberation Army Air Force Algerian Air Force[source] |
|---|
| Number built | 600+ (As of 2024 )[source] | 630+ (as of 2019 )[source] |
|---|
| Manufactured | 2002–present[source] | 1992–present[source] |
|---|
| Introduction date | 2004[source] | 1992 (Su-30) 2013 (Su-30SM)[source] |
|---|
| First flight | 23 March 1998[source] | 31 December 1989 ( 1989-12-31 )[source] |
|---|
| Developed from | Chengdu J-9[source] | Sukhoi Su-27[source] |
|---|
| Fuel capacity | 4000 L (3120 kg) external with 3 drop tanks (2 × 1600L + 1 × 800L)[source] | 9,400 kg (20,723 lb) internal[source] |
|---|
| Guns | 1× Gryazev-Shipunov GSh-23[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Hardpoints | 11 in total (6 × under-wing, 2 × under-intake and 3 × under-fuselage) with a capacity of 5600 kg of external fuel and ordnance[source] | 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] |
|---|
| Stall speed | 200 km/h (120 mph, 110 kn)[source] | — |
|---|
| Wing loading | 381 kg/m 2 (78 lb/sq ft)[source] | 401 kg/m 2 (82 lb/sq ft) with 56% fuel[source] |
|---|
| Thrust/weight | 1.04[source] | 1 with 56% fuel[source] |
|---|
| Rockets | 90 mm unguided rocket pods[source] | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
| Missiles | Air-to-air missiles : PL-8 short-range air-to-air missile PL-10 short-range air-to-air missile (J-10C) PL-12 BVR air-to-air missile PL-15 BVR air-to-air missile (J-10C) PL-17 BVR air-to-air missile (modified J-10C with DF-4/3 external pylons) Air-to-surface missiles : KD-88 standoff land attack missile YJ-91 anti-radiation missile Anti-ship missiles : YJ-83 K anti-ship cruise missile YJ-21 anti-ship ballistic missile (ongoing integration process for J-10C)[source] | 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 | PL-8 short-range air-to-air missile PL-10 short-range air-to-air missile (J-10C) PL-12 BVR air-to-air missile PL-15 BVR air-to-air missile (J-10C) PL-17 BVR air-to-air missile (modified J-10C with DF-4/3 external pylons)[source] | — |
|---|
| Air-to-surface missiles | KD-88 standoff land attack missile YJ-91 anti-radiation missile[source] | — |
|---|
| Anti-ship missiles | YJ-83 K anti-ship cruise missile YJ-21 anti-ship ballistic missile (ongoing integration process for J-10C)[source] | — |
|---|
| Bombs | Laser-guided bombs: (LS-500J, LT-2 ) Glide bombs: ( LS-6 , GB3 , GB2A , GB3A , GB250 ) Satellite-guided bombs: ( FT-1 ) Unguided bombs: 250 kg, 500 kg[source] | 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] |
|---|
| Others | Up to 3 external fuel drop-tanks (1 × under-fuselage, 2 × under-wing) for extended range and loitering time[source] | — |
|---|
| Built by | — | KnAAPO Irkut Corporation Hindustan Aeronautics Limited (built by HAL in India under license)[source] |
|---|
| Variants | — | Sukhoi Su-30MKI Sukhoi Su-30MKK Sukhoi Su-30MKM Sukhoi Su-30MKA[source] |
|---|
| g limits | — | + 9[source] |
|---|
2 × 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]