FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
KAAN development aircraft; manufacturer technical data, configuration not stated · Length
Single sourcePreliminary specifications (KAAN development aircraft) · Length
Single sourceConfiguration
| Specification | TAI TF Kaan | Tupolev Tu-95 |
|---|---|---|
| Crew | One[source]Preliminary specifications; development aircraft, not a verified production Block 10 configuration | 6–7; pilot, co-pilot, flight engineer, communications system operator, navigator, tail gunner, plus additional navigator, depending on mission profile.[source] |
| Other name | TF or MMU[source] | — |
| Type | Stealth multirole / air superiority fighter[source] | Strategic heavy nuclear bomber[source] |
| National origin | Turkey[source] | Soviet Union |
20.3 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
Tu-95MS · Length
Single source46.2 m (151 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
Tu-95MS · Wingspan
Single source50.1 m (164 ft 4 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
Tu-95MS · Height
Single source12.12 m (39 ft 9 in)[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
Empty; Tu-95MS · Empty weight
Single sourceGross; Tu-95MS · Gross weight
Single sourceTu-95MS · Range
Single source15,000 km (9,300 mi, 8,100 nmi)[source]
Tu-95MS · 4 × Kuznetsov NK-12 turboprop engines
Single source4 × Kuznetsov NK-12 turboprop engines 15,000 PS (15,000 hp; 11,000 kW)[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 source2 × 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
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
Tu-95MS · Wing area
Single source310 m 2 (3,300 sq 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
Tu-95MS · Service ceiling
Single source13,716 m (45,000 ft)[source]
Tu-95MS · 2,000 ft/min
Single source10 m/s (2,000 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufacturer | Turkish Aerospace Industries[source] | Aviakor[source] |
|---|
| Designer | BAE Systems TAI[source] | Tupolev[source] |
|---|
| Status | Under development[source] | In service[source] |
|---|
| Primary user | Turkish Air Force[source] | — |
|---|
| Prototypes | — |
|---|
| Flights | — |
|---|
| Introduction date | 2030s (planned)[source] | 1956[source] |
|---|
| First flight | 21 February 2024[source] | 12 November 1952 ( 1952-11-12 )[source] |
|---|
| 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 | 606 kg/m 2 (124 lb/sq ft)[source] |
|---|
| Thrust/weight | 0,75[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 | 2 × 23 mm (0.906 in) Gryazev-Shipunov GSh-23 autocannon in tail turret[source] |
|---|
| 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 | Up to 15,000 kg (33,000 lb), including the Kh-20 , Kh-22 , and Kh-55/101/102 , or 8 Kh-101/102 cruise missiles mounted on underwing pylons.[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 | — |
|---|
| Primary users | — | Russian Aerospace Forces Soviet Air Forces (historical) Soviet Navy (historical) Ukrainian Air Force (historical)[source] |
|---|
| Number built | — | >500[source] |
|---|
| Manufactured | — | 1952–1993[source] |
|---|
| Variants | — | Tupolev Tu-114 Tupolev Tu-142 Tupolev Tu-95LAL Tupolev Tu-116[source] |
|---|
| Fuel capacity | — | 148,150 lb (67,200 kg)[source] |
|---|
| Propellers | — | 8-bladed contra-rotating fully feathering constant-speed propellers[source] |
|---|
| Power/mass | — | 0.235 kW/kg (0.143 hp/lb)[source] |
|---|
Maximum take-off; Tu-95MS · Max takeoff weight
Single source