Credit
Peng Chen · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
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At a glance
Measured figures
J-5A · Length · source measurement 1
Single sourceJ-5A · Length · source measurement 2
Single sourceConfiguration
| Specification | Shenyang J-5 | TAI TF Kaan |
|---|---|---|
| Type | Fighter aircraft[source] | Stealth multirole / air superiority fighter[source] |
| National origin | People's Republic of China[source] | Turkey[source] |
| Manufacturer | Shenyang Aircraft Corporation[source] | Turkish Aerospace Industries[source] |
| Status | In service with North Korea[source] | Under development |
11.09 m (36 ft 5 in) 11.36 m (37.3 ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourcePreliminary 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
J-5A · Wingspan
Single source9.628 m (31 ft 7 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
J-5A · Height
Single source3.8 m (12 ft 6 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; J-5A · Empty weight · source measurement 1
Single sourceEmpty; J-5A · Empty weight · source measurement 2
Single sourceGross; J-5A · Gross weight · source measurement 1
Single sourceGross; J-5A · Gross weight · source measurement 2
Single source3,939 kg (8,684 lb) 4,151 kg (9,151 lb)[source]
6,000 kg (13,228 lb) 6,125 kg (13,503 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; J-5A · at 5,000 m (16,000 ft)
Single sourceMaximum; J-5A · Maximum speed
Single source1,130 km/h (700 mph, 610 kn) at 5,000 m (16,000 ft): 1,145 km/h (711 mph; 618 kn)[source]
J-5A · Range
Single sourceJ-5A · with drop tanks at 10,000 m (33,000 ft)
Single source1,424 km (885 mi, 769 nmi) with drop tanks at 10,000 m (33,000 ft): 1,730 km (1,070 mi; 930 nmi)[source]
J-5A · 1 × Wopen WP-5 turbojet engine thrust
Single sourceJ-5A · with afterburning
Single source1 × Wopen WP-5 turbojet engine, 25.5 kN (5,700 lbf) thrust 33.8 kN (7,600 lbf) with afterburning[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 sourceJ-5A · Wing area
Single source22.6 m 2 (243 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
J-5A · Service ceiling · source measurement 1
Single sourceJ-5A · Service ceiling · source measurement 2
Single source16,500 m (54,100 ft) 16,600 m (54,500 ft)[source]
KAAN development aircraft; manufacturer technical data, configuration not stated · Service ceiling
Manufacturer claimPreliminary specifications (KAAN development aircraft) · Service ceiling
Single sourceJ-5A · (12,800 ft/min) at 5,000 m (16,000 ft)
Single sourceJ-5A · 5,300 ft/min
Single source65 m/s (12,800 ft/min) at 5,000 m (16,000 ft): 27 m/s (5,300 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | People's Liberation Army Air Force (historical) Korean People's Army Air Force Pakistan Air Force (historical) Vietnam People's Air Force (historical)[source] | — |
|---|
| Number built | 1,820+[source] | — |
|---|
| Manufactured | 1956–1969[source] | — |
|---|
| Introduction date | 1957[source] | 2030s (planned)[source] |
|---|
| First flight | 19 July 1956[source] | 21 February 2024[source] |
|---|
| Retired | 1992 (China)[source] | — |
|---|
| Developed from | Mikoyan-Gurevich MiG-17[source] | — |
|---|
| Guns | 3 x Type 23-1 23 mm (0.906 in) aircraft cannon[source] | 30x113 mm[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 |
|---|
| Wing loading | — | 485 kg/m 2 (99 lb/sq ft)[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 |
|---|
| Hardpoints | — | 8 internal; 3 per wing, total 6 external[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration |
|---|
| Missiles | — | 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 | — | 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