Credit
TSGT CURT EDDINGS · Public domain · Resized · Public domain · Source ↗ · Modified
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At a glance
Measured figures
Mirage IIIE · Length
Single source15.03 m (49 ft 4 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Configuration
| Specification | Dassault Mirage III | TAI TF Kaan |
|---|---|---|
| Type | Interceptor aircraft[source] | Stealth multirole / air superiority fighter[source] |
| National origin | France[source] | Turkey[source] |
| Manufacturer | Dassault Aviation[source] | Turkish Aerospace Industries[source] |
| Status | In service with the Pakistan Air Force[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 IIIE · Wingspan
Single source8.22 m (27 ft 0 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 IIIE · Height
Single source4.5 m (14 ft 9 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 IIIE · Empty weight
Single sourceGross; Mirage IIIE · Gross weight
Single sourceMaximum take-off; Mirage IIIE · Max takeoff weight
Single source7,050 kg (15,543 lb)[source]
9,600 kg (21,164 lb)[source]
13,700 kg (30,203 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 IIIE · at 12,000 m (39,000 ft)
Single source2,350 km/h (1,460 mph, 1,270 kn) at 12,000 m (39,000 ft)[source]
Ferry; Mirage IIIE · Ferry range
Single source3,335 km (2,072 mi, 1,801 nmi)[source]
Mirage IIIE · Combat range
Single source1,200 km (750 mi, 650 nmi)[source]
Mirage IIIE · 1 × SNECMA Atar 09C afterburning turbojet engine thrust dry
Single sourceMirage IIIE · with afterburner
Single source1 × SNECMA Atar 09C afterburning turbojet engine, 41.97 kN (9,440 lbf) thrust dry, 60.8 kN (13,700 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 IIIE · Wing area
Single source34.85 m 2 (375.1 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 IIIE · Service ceiling
Single source17,000 m (56,000 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 IIIE · 16,400 ft/min
Single source83 m/s (16,400 ft/min)[source]
Mirage IIIE · Bombs of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks ; French Air Force IIIEs through to 1991 were equipped to carry the AN-52 nuclear bomb
Single sourceBombs: 4,000 kg (8,800 lb) of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks ; French Air Force IIIEs through to 1991 were equipped to carry the AN-52 nuclear bomb.[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | French Air Force (historical) Royal Australian Air Force (historical) Pakistan Air Force Israeli Air Force (historical)[source] | — |
|---|
| Number built | 1,422[source] | — |
|---|
| Introduction date | 1961[source] | 2030s (planned)[source] |
|---|
| First flight | 17 November 1956[source] | 21 February 2024[source] |
|---|
| Variants | Dassault Mirage IIIV Dassault Mirage 5 Atlas Cheetah[source] | — |
|---|
| Guns | 2 × 30 mm (1.181 in) DEFA 552 cannon with 125 rounds per gun[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Wing loading | 275 kg/m 2 (56.4 lb/sq ft)[source] | 485 kg/m 2 (99 lb/sq ft)[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Rockets | 2 × Matra JL-100 drop tank/rocket pack, each with 19× 68 mm (2.7 in) SNEB rockets and 250 L (66 US gal; 55 imp gal) of fuel[source] | — |
|---|
| Missiles | 2 × AIM-9B Sidewinder Air to Air missiles (AAM) or 2 × Matra R.550 Magic AAMs plus 1× Matra R.530 AAM[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 |
|---|
| Bombs | 4,000 kg (8,800 lb) of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks ; French Air Force IIIEs through to 1991 were equipped to carry the AN-52 nuclear bomb.[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 |
|---|
| Hardpoints | Bombs: 4,000 kg (8,800 lb) of payload on five external hardpoints , including a variety of bombs, reconnaissance pods or Drop tanks ; French Air Force IIIEs through to 1991 were equipped to carry the AN-52 nuclear bomb.[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] |
|---|
| Primary user | — | Turkish Air Force[source] |
|---|
| Prototypes | — |
|---|
| Flights | — |
|---|
| Initiated | — | 2010[source] |
|---|
| g limits | — | +9,0 g & −3,5 g[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Thrust/weight | — | 0,75[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 |
|---|
| Reported operators |
| — |
|---|
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