Credit
Rob Schleiffert from Holland · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Mirage 2000D/N · Length
Single source14.55 m (47 ft 9 in)[source]
Su-27PU/Su-30 · Length
Configuration
| Specification | Dassault Mirage 2000N/2000D | Sukhoi Su-30 |
|---|---|---|
| Type | Multirole combat aircraft[source] | Multirole fighter[source] |
| National origin | France[source] | Soviet Union Russia[source] |
| Manufacturer | Dassault Aviation[source] | Sukhoi, Komsomolsk-on-Amur Aircraft Production Association, Yakovlev Corporation[source] |
| Status | Active (2000D only)[source] |
21.935 m (72 ft 0 in)[source]
Empty; Mirage 2000D/N · Empty weight
Single sourceGross; Mirage 2000D/N · Gross weight
Single sourceMaximum take-off; Mirage 2000D/N · Max takeoff weight
Single source7,600 kg (16,755 lb)[source]
10,680 kg (23,545 lb)[source]
17,000 kg (37,479 lb)[source]
Empty; Su-27PU/Su-30 · Empty weight
Single sourceGross; Su-27PU/Su-30 · Gross weight
Single sourceMirage 2000D/N · Combat range
Single source1,480 km (920 mi, 800 nmi)[source]
Mirage 2000D/N · 1 × SNECMA M53-P2 afterburning turbofan engine thrust dry
Single sourceMirage 2000D/N · with afterburner
Single source1 × SNECMA M53-P2 afterburning turbofan engine, 64 kN (14,000 lbf) thrust dry, 95.1 kN (21,400 lbf) 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 sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
In service[source]
| Primary user | French Air and Space Force[source] | — |
|---|
| Number built | 161 (75 Mirage 2000N and 86 Mirage 2000D)[source] | 630+ (as of 2019 )[source] |
|---|
| First flight | 3 February 1986[source] | 31 December 1989 ( 1989-12-31 )[source] |
|---|
| Retired | 2018 (2000N)[source] | — |
|---|
| Developed from | Mirage 2000[source] | Sukhoi Su-27[source] |
|---|
| Wing loading | 410 kg/m 2 (84 lb/sq ft)[source] | 401 kg/m 2 (82 lb/sq ft) with 56% fuel[source] |
|---|
| Thrust/weight | * Propulsive efficiency: 0.91 (non dimensional)[source] | 1 with 56% fuel[source] |
|---|
| Rockets | Up to 4× Matra SNEB 68-mm 18-round rocket pods on the four underwing hardpoints[source] | S-8 KOM/BM/OM S-13 T/OF S-25 OFM-PU[source] |
|---|
| Missiles | Air-to-air missiles : Up to 4× R550 Magic air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons Up to 6× MICA air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons Air-to-surface missiles : – Mirage 2000N 1× ASMP medium-range nuclear missile on the centerline pylon Air-to-surface missiles : – Mirage 2000D 1× Apache anti-runway cruise missile on the centerline pylon 1× SCALP EG air-launched cruise missile on the centerline pylon 2× AS-30L laser-guided missiles on the inboard underwing pylons[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 | Up to 4× R550 Magic air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons Up to 6× MICA air-to-air missiles for self-defence, normally 2 on the outboard underwing pylons[source] | — |
|---|
| Air-to-surface missiles | – Mirage 2000N 1× ASMP medium-range nuclear missile on the centerline pylon[source] | — |
|---|
| Bombs | AASM 125, 250, 1000 Kg laser, ISN/GPS, IIR guided bombs. The lighter versions are carried in pairs on the centerline and inboard wing hardpoints and one under each of the four fuselage hardpoints up to 10× GBU-12 227 Kg laser-guided bombs or GBU-49 227 Kg INS/GPS and laser guided bombs, in pairs on the centerline and inboard wing hardpoints and one under each of the four fuselage hardpoints up to 3× GBU-16 454 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× GBU-10 907 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× GBU-24 907 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× BGL-400 400 Kg laser-guided bombs on the centerline and inboard wing hardpoints up to 3× BGL-1000 1000 Kg laser-guided bombs on the centerline and inboard wing hardpoints[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] |
|---|
| Other | ATLIS II laser/electro-optical targeting pod on the front-right fuselage hardpoint PDLCT laser/electro-optical targeting pod on the front-right fuselage hardpoint Damoclès laser targeting pod on the front-right fuselage hardpoint 1× centerline mounted 345-gallon drop tank 2x either 375, 440 or 530 gallon tanks for ferry flight/extended range/loitering time up to 2× 30 mm CC630 gun pods with 600 rounds per pod, one on each inboard wing hardpoint[source] | — |
|---|
| Hardpoints | 4× under-wing, 4× under fuselage, 1× centerline , with provisions to carry combinations of:[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] |
|---|
| Designer | — | Sukhoi[source] |
|---|
| Built by | — | KnAAPO Irkut Corporation Hindustan Aeronautics Limited (built by HAL in India under license)[source] |
|---|
| Primary users | — | Russian Aerospace Forces Indian Air Force People's Liberation Army Air Force Algerian Air Force[source] |
|---|
| Manufactured | — | 1992–present[source] |
|---|
| Introduction date | — | 1992 (Su-30) 2013 (Su-30SM)[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] |
|---|
| Guns | — | 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds[source] |
|---|
| g limits | — | + 9[source] |
|---|
Maximum take-off; Su-27PU/Su-30 · Max takeoff weight
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]