TAI/AgustaWestland T129 ATAK | |
|---|---|
| Land | Turkiet och Italien |
| Roll | Attackhelikopter |
| Första flygningen | den 28 september 2009 |
| Byggd | 75+ |
Den TAI/AgustaWestland T129 ATAK is a twin-engine, tandem seat, multi-role, all-weather attack helicopter based on the Agusta A129 Mangusta platform. The T129 was developed by Turkish Aerospace Industries (TAI) with partner AgustaWestland. The helicopter is designed for advanced attack and reconnaissance missions in hot and high environments and rough geography in both day and night conditions. The ATAK programme was begun to meet the Turkish Armed Forces’ requirements for an attack and tactical reconnaissance helicopter. The T129 is the result of the integration of Turkish-developed avionics, airframe modifications, and weapon systems onto the AgustaWestland A129 airframe, with upgraded engines, transmission and rotor blades. It is in use by the Turkish Army and other services including the Turkish Gendarmerie.
| T-129 Atak Walk Around | |
|---|---|
| Fotograf | Chadi Rachid |
| Lokalisering | Unknow |
| Bilder | 67 |
| TAI T-129 Atak Walk Around | |
|---|---|
| Fotograf | Unknow |
| Lokalisering | Unknow |
| Bilder | 22 |
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General Characteristics
The T129 ATAK (Attack and Tactical Reconnaissance Helicopter) is a twin-engine, tandem-seat, multi-role attack helicopter developed by Turkish Aerospace Industries (TAI) and AgustaWestland (now Leonardo), based on the A129 Mangusta.
| Property | Value (T129 ATAK) |
|---|---|
| Roll | Multi-Role Attack, Reconnaissance |
| Tillverkare | TAI / AgustaWestland (Leonardo) |
| Maiden Flight | September 2009 |
| besättning | 2 (Pilot and Co-Pilot/Gunner in tandem seats) |
| Maximum Take-Off Weight | 5,000 kg (11,023 lb) |
| Design Focus | Optimized for “hot and high” conditions and rough geography. |
Powerplant and Performance
- Powerplant: Two LHTEC CTS800-4A turboshaft engines.
- Power Output: 1,014 kW (1,361 hp) each.
- Maximum Cruise Speed: 269 km/h (167 mph / 145 knots).
- Range: 561 km (349 miles).
- Ferry Range: 1,000 km (620 miles).
- Service Ceiling: 6,096 m (20,000 ft).
- Engine Control: Features Full Authority Digital Engine Control (FADEC) for efficient operation.
Armament and Avionics
- Cannon: One M197 20 mm three-barrel rotary cannon (500 rounds) mounted on a nose turret.
- Hardpoints: Four underwing hardpoints with a total payload capacity of 1,200 kg.
- Anti-Tank Missiles: Roketsan UMTAS (Long Range Anti-Tank Missile System).
- Guided Rockets: Roketsan Cirit 70 mm Laser Guided Rockets (LGR).
- Air-to-Air Missiles: AIM-92 Stinger (ATAS).
- Avionics: Integrated survivability suite including Radar Warning Receiver (RWR), Laser Warning System, and flare/chaff dispensers.
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