Credit
Rob Schleiffert from Holland · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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At a glance
Measured figures
Mirage 2000D/N · Length
Single source14.55 m (47 ft 9 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Configuration
| Specification | Dassault Mirage 2000N/2000D | TAI TF Kaan |
|---|---|---|
| Type | Multirole combat aircraft[source] | Stealth multirole / air superiority fighter[source] |
| National origin | France[source] | Turkey[source] |
| Manufacturer | Dassault Aviation[source] | Turkish Aerospace Industries[source] |
| Status | Active (2000D only)[source] | Under development |
Preliminary specifications (KAAN development aircraft) · Length
Single source20.3 m (66 ft 7 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
20,3 m (66 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Mirage 2000D/N · Wingspan
Single source9.13 m (29 ft 11 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Wingspan
Single sourcePreliminary specifications (KAAN development aircraft) · Wingspan
Single source13.4 m (44 ft 0 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
13,4 m (44 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Mirage 2000D/N · Height
Single source5.15 m (16 ft 11 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Height
Single sourcePreliminary specifications (KAAN development aircraft) · Height
Single source5 m (16 ft 5 in)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
5 m (16 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
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]
Maximum take-off; Preliminary specifications (KAAN development aircraft) · Maximum takeoff weight
Single source34,750 kg (76,500 lb)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
34.750 kg (76,500 lb)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Maximum; Mirage 2000D/N · Maximum speed
Single source1,728 km/h (1,074 mph, 933 kn)[source]
Ferry; Mirage 2000D/N · Ferry range
Single source3,340 km (2,080 mi, 1,800 nmi)[source]
Mirage 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]
Preliminary specifications (KAAN development aircraft) · 2 × General Electric F110-GE-129 Turbofan thrust each dry
Single sourcePreliminary specifications (KAAN development aircraft) · with afterburner
Single sourceMirage 2000D/N · Wing area
Single source41 m 2 (440 sq ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Wing area
Single sourcePreliminary specifications (KAAN development aircraft) · Wing area
Single source71.6 m 2 (770 sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
71,6 m2 (771 ft2)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Mirage 2000D/N · Service ceiling
Single source18,000 m (59,000 ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Service ceiling
Manufacturer claimPreliminary specifications (KAAN development aircraft) · Service ceiling
Single source16,764 m (55,000 ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
16.764 m (55,000 ft)[source]KAAN development aircraft; manufacturer technical data, configuration not stated
Mirage 2000D/N · 56,100 ft/min
Single source285 m/s (56,100 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | French Air and Space Force[source] | Turkish Air Force[source] |
|---|
| Number built | 161 (75 Mirage 2000N and 86 Mirage 2000D)[source] | — |
|---|
| First flight | 3 February 1986[source] | 21 February 2024[source] |
|---|
| Retired | 2018 (2000N)[source] | — |
|---|
| Developed from | Mirage 2000[source] | — |
|---|
| Wing loading | 410 kg/m 2 (84 lb/sq ft)[source] | 485 kg/m 2 (99 lb/sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Thrust/weight | * Propulsive efficiency: 0.91 (non dimensional)[source] | 0,75[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Rockets | Up to 4× Matra SNEB 68-mm 18-round rocket pods on the four underwing hardpoints[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 : GÖKTUĞ missile program: Gökdoğan BVR active radar homing Gökhan ramjet engine powered BVR active radar homing Bozdoğan short-range infrared homing Air-to-surface missiles : SOM Cruise Missile (B1, B2, and J variants) KUZGUN-TJ, Turbojet-powered Air-to-surface missile KUZGUN-KY, Solid fuel Rocket-powered Air-to-surface missile KUZGUN-ER, Turbojet-powered , Air-to-surface missile (According to TUBITAK-SAGE, this missile will be equivalent to Penguin Missiles .) KUZGUN-EW, KUZGUN-EW will be able to carry miniaturised EW payload which will act as a stand-in jammer and suppress enemy air defences to significantly increase the survivability of the aircraft of the Turkish Air Force . AKBABA, Air-to-surface , Anti-radiation Missile (ARM) ROKETSAN ÇAKIR Missile Family , Anti-ship , Air-to-surface , surface-to-surface Cruise Missile .[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| 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] | Teber-81 ( Mark 81 bomb w/ ROKETSAN Laser Guidance Kit) HGK-82 ( Mark 82 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) KGK-82 ( Mark 82 bomb w/ TUBITAK-SAGE Wing Assisted Guidance Kit) Teber-82 ( Mark 82 bomb w/ ROKETSAN Laser Guidance Kit) HGK-83 ( Mark 83 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) KGK-83 ( Mark 83 bomb w/ TUBITAK-SAGE Wing Assisted Guidance Kit) HGK-84 ( Mark 84 bomb w/ TUBITAK-SAGE Precision Guidance Kit ) LHGK-84 ( Mark 84 bomb w/ TUBITAK-SAGE Laser Sensitive Guidance Kit) SARB-83, Bunker buster NEB-84, Bunker buster MAM (Smart Micro Munition) (MAM-T variant) KUZGUN-SS, Glide bomb ASELSAN Miniature Bomb[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| 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] | 8 internal; 3 per wing, total 6 external[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Other name | — | TF or MMU[source] |
|---|
| Designer | — | BAE Systems TAI[source] |
|---|
| Prototypes | — |
|---|
| Flights | — |
|---|
| Introduction date | — | 2030s (planned)[source] |
|---|
| Initiated | — | 2010[source] |
|---|
| g limits | — | +9,0 g & −3,5 g[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Guns | — | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated RF System (IRFS) | — | MURAD-600A AESA radar Radar warning receiver[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated Electro-Optical System (IEOS) | — | KARAT-200 Infrared Search and Track (IRST) TOYGUN Electro-optical reconnaissance, surveillance and targeting system İRİS-300 Missile approach warning system (IR-MWS/360° day/night imaging) YILDIRIM-300 Directional Infrared Counter Measures (DIRCM) LİAS-300 Laser warning receiver (LWS)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Integrated Communications Navigation and IFF (ICNI) | — | ICNAir-ASQ9683 communications suite ARVEN radio-navigation equipment IdentIFF Mode-5 identification friend or foe[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Advanced Cockpit / Human Machine Interface | — | TULGAR Helmet-mounted display (HMDS) LAD-208 Large area display (LAD)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Positive / Negative G Limit | — | +9 / -3,5 G[source]KAAN development aircraft; manufacturer technical data, configuration not stated |
|---|
2 × General Electric F110-GE-129 Turbofan , 76.3 kN (17.155 lbf) thrust each dry, 131 kN (29,000 lbf) with afterburner[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration
2 x 13.150 kgf (2 x 29,000 lb)[source]KAAN development aircraft; manufacturer technical data, configuration not stated