Credit
Vitaly Kuzmin · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
MiG-31 · Length
Single source22.62 m (74 ft 3 in)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourceConfiguration
| Specification | Mikoyan MiG-31 | TAI TF Kaan |
|---|---|---|
| Type | Interceptor aircraft , strike fighter[source] | Stealth multirole / air superiority fighter[source] |
| National origin | Soviet Union[source] | Turkey[source] |
| Manufacturer | Mikoyan-Gurevich/Mikoyan[source] | Turkish Aerospace Industries[source] |
| Status | In service with the Russian 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
MiG-31 · Wingspan
Single source13.456 m (44 ft 2 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
MiG-31 · Height
Single source6.456 m (21 ft 2 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; MiG-31 · Empty weight
Single sourceGross; MiG-31 · Gross weight
Single sourceMaximum take-off; MiG-31 · Max takeoff weight
Single source21,820 kg (48,105 lb)[source]
41,000 kg (90,390 lb)[source]
46,200 kg (101,854 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
MiG-31 · with 4 × R-33E and 2 drop tanks
Single source3,000 km (1,900 mi, 1,600 nmi) with 4 × R-33E and 2 drop tanks[source]
MiG-31 · at Mach 0.8 and
Single sourceMiG-31 · Combat range
Single source1,450 km (900 mi, 780 nmi) at Mach 0.8 and 10,000 m (33,000 ft)[source]
MiG-31 · 2 × Soloviev D-30 F6 afterburning turbofan engines thrust each dry
Single sourceMiG-31 · with afterburner
Single source2 × Soloviev D-30 F6 afterburning turbofan engines, 93 kN (21,000 lbf) thrust each dry, 152 kN (34,000 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 sourceMiG-31 · Wing area
Single source61.6 m 2 (663 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
MiG-31 · +
Single source25,000 m (82,000 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
MiG-31 · 56,700 ft/min
Single source288 m/s (56,700 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | Russian Aerospace Forces Kazakh Air Defense Forces (historical)[source] | — |
|---|
| Number built | 519[source] | — |
|---|
| Manufactured | 1975–1994[source] | — |
|---|
| Introduction date | 6 May 1981[source] | 2030s (planned)[source] |
|---|
| First flight | 16 September 1975 ( 1975-09-16 )[source] | 21 February 2024[source] |
|---|
| Retired | 2023 (Kazakh Air Force)[source] | — |
|---|
| Developed from | Mikoyan-Gurevich MiG-25[source] | — |
|---|
| Fuel capacity | 35,550 lb (16,130 kg) internals, plus optional external fuel tanks[source] | — |
|---|
| Guns | 1 × 23 mm Gryazev-Shipunov GSh-6-23 M rotary cannon with 260 rounds.[source] | 30x113 mm[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Hardpoints | 4 × semi-recessed under the fuselage and 4 × underwing pylons with capacity of up to 9,000 kg (20,000 lb) of ordnance , with provisions to carry combinations of: Missiles: Air-to-air missiles : 4 × R-33 2 × R-40 RD/TD 4 × R-60 MK 4 × R-73 4 × R-77 4 × R-37 M (MiG-31BM only) 4 × R-77 M (MiG-31BM only)[source] | 8 internal; 3 per wing, total 6 external[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| g limits | 5+[source] | +9,0 g & −3,5 g[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Wing loading | 665 kg/m 2 (136 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 | 0.85[source] | 0,75[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Missiles | Air-to-air missiles :[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 |
|---|
| Other name | — | TF or MMU[source] |
|---|
| Designer | — | BAE Systems TAI[source] |
|---|
| Primary user | — | Turkish Air Force[source] |
|---|
| Prototypes | — |
|---|
| Flights | — |
|---|
| Initiated | — | 2010[source] |
|---|
| Bombs | — | 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 |
|---|
| 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