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Wisnia6522 · Public domain · Resized · Public domain · Source ↗ · Modified
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At a glance
Measured figures
Il-28 · Length
Single source17.65 m (57 ft 11 in)[source]
Su-27PU/Su-30 · Length
Single sourceConfiguration
| Specification | Ilyushin Il-28 | Sukhoi Su-30 |
|---|---|---|
| Type | Medium bomber[source] | Multirole fighter[source] |
| National origin | Soviet Union[source] | Soviet Union Russia[source] |
| Manufacturer | Ilyushin Harbin Aircraft Manufacturing Corporation (H-5)[source] | Sukhoi, Komsomolsk-on-Amur Aircraft Production Association, Yakovlev Corporation[source] |
| Status | In service with the Korean People's Air Force[source] | In service |
21.935 m (72 ft 0 in)[source]
Empty; Il-28 · Empty weight
Single sourceGross; Il-28 · Gross weight
Single sourceMaximum take-off; Il-28 · Max takeoff weight
Single source12,890 kg (28,418 lb)[source]
18,400 kg (40,565 lb)[source]
21,200 kg (46,738 lb)[source]
Empty; Su-27PU/Su-30 · Empty weight
Single sourceGross; Su-27PU/Su-30 · Gross weight
Single sourceCruise; Il-28 · at 10,000 m (33,000 ft)
Single sourceMaximum; Il-28 · at 4,500 m (14,800 ft)
Single source902 km/h (560 mph, 487 kn) at 4,500 m (14,800 ft)[source]
770 km/h (480 mph, 420 kn) at 10,000 m (33,000 ft)[source]
Maximum; Su-27PU/Su-30 · at high altitude
Single source2,120 km/h (1,320 mph, 1,140 kn) at high altitude[source]
Il-28 · 2 × Klimov VK-1A centrifugal-flow turbojet engines thrust each
Single source2 × Klimov VK-1A centrifugal-flow turbojet engines, 26.5 kN (6,000 lbf) thrust each[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Soviet Air Force People's Liberation Army Air Force Czechoslovak Air Force Polish Air Force[source] | Russian Aerospace Forces Indian Air Force People's Liberation Army Air Force Algerian Air Force[source] |
|---|
| Number built | over 6,635[source] | 630+ (as of 2019 )[source] |
|---|
| Introduction date | 1950[source] | 1992 (Su-30) 2013 (Su-30SM)[source] |
|---|
| First flight | 8 July 1948[source] | 31 December 1989 ( 1989-12-31 )[source] |
|---|
| Retired | 1980s (Soviet Union)[source] | — |
|---|
| Developed into | Ilyushin Il-30[source] | — |
|---|
| Guns | 4 × Nudelman-Rikhter NR-23 cannons (2 in nose and 2 in tail barbette )[source] | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| Airfoil | TsAGI SR-5S (12%)[source] | — |
|---|
| Bombs | 3,000 kg (6,600 lb) of bombs in internal bay (1,000 kg (2,200 lb) normal)[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] |
|---|
| Designer | — | Sukhoi[source] |
|---|
| Built by | — | KnAAPO Irkut Corporation Hindustan Aeronautics Limited (built by HAL in India under license)[source] |
|---|
| Manufactured | — | 1992–present[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] |
|---|
| 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] |
|---|
| g limits | — | + 9[source] |
|---|
| Wing loading | — | 401 kg/m 2 (82 lb/sq ft) with 56% fuel[source] |
|---|
| Thrust/weight | — | 1 with 56% 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] |
|---|
Maximum take-off; Su-27PU/Su-30 · Max takeoff weight
Single source