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]
Tu-95MS · Length
Single sourceConfiguration
| Specification | Sukhoi Su-30 | Tupolev Tu-95 |
|---|---|---|
| Type | Multirole fighter[source] | Strategic heavy nuclear bomber[source] |
| National origin | Soviet Union Russia[source] | Soviet Union[source] |
| Designer | Sukhoi[source] | Tupolev[source] |
| Built by | KnAAPO Irkut Corporation Hindustan Aeronautics Limited (built by HAL in India under license)[source] | — |
46.2 m (151 ft 7 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; Tu-95MS · Empty weight
Single sourceGross; Tu-95MS · Gross weight
Single sourceTu-95MS · 4 × Kuznetsov NK-12 turboprop engines
Single source4 × Kuznetsov NK-12 turboprop engines 15,000 PS (15,000 hp; 11,000 kW)[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.
| 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 Soviet Air Forces (historical) Soviet Navy (historical) Ukrainian Air Force (historical)[source] |
|---|
| Number built | 630+ (as of 2019 )[source] | >500[source] |
|---|
| Manufactured | 1992–present[source] | 1952–1993[source] |
|---|
| Introduction date | 1992 (Su-30) 2013 (Su-30SM)[source] | 1956[source] |
|---|
| First flight | 31 December 1989 ( 1989-12-31 )[source] | 12 November 1952 ( 1952-11-12 )[source] |
|---|
| Developed from | Sukhoi Su-27[source] | — |
|---|
| Variants | Sukhoi Su-30MKI Sukhoi Su-30MKK Sukhoi Su-30MKM Sukhoi Su-30MKA[source] | Tupolev Tu-114 Tupolev Tu-142 Tupolev Tu-95LAL Tupolev Tu-116[source] |
|---|
| Fuel capacity | 9,400 kg (20,723 lb) internal[source] | 148,150 lb (67,200 kg)[source] |
|---|
| Guns | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] | 2 × 23 mm (0.906 in) Gryazev-Shipunov GSh-23 autocannon in tail turret[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] | 606 kg/m 2 (124 lb/sq ft)[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] | Up to 15,000 kg (33,000 lb), including the Kh-20 , Kh-22 , and Kh-55/101/102 , or 8 Kh-101/102 cruise missiles mounted on underwing pylons.[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] | — |
|---|
| Manufacturer | Sukhoi, Komsomolsk-on-Amur Aircraft Production Association, Yakovlev Corporation[source] | Aviakor[source] |
|---|
| Propellers | — | 8-bladed contra-rotating fully feathering constant-speed propellers[source] |
|---|
| Power/mass | — | 0.235 kW/kg (0.143 hp/lb)[source] |
|---|
Maximum take-off; Tu-95MS · Max takeoff weight
Single source