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TAI T925

Turkish heavy utility helicopter From Wikipedia, the free encyclopedia

The TAI T925 is a twin-engined heavy transport/utility helicopter developed by Turkish Aerospace Industries.[1]

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T925
General information
Typeheavy multirole helicopter
National originTurkey
ManufacturerTurkish Aerospace Industries
DesignerTurkish Aerospace Industries
Statusin design
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Design and development

The mock-up of helicopter was firstly presented at Paris Air Show 2023.[2]

The helicopter is planned to be made in VIP transport version, transport version for troops and equipment, naval version, search and rescue, firefighting, medical transport.[3]

The T925 will be unveiled in its final configuration by the end of this year. Its first flight is planned for the first quarter of 2027.[4][5]

Operators

Future operators

 Turkey

General characteristics

  • Crew: 2
  • Capacity: 19 passengers / troops
  • Length: 19.95–20.2 m (65 ft 5 in – 66 ft 3 in)
  • Height: 3.8 m (12 ft 6 in)
  • Max takeoff weight: 11,500–12,000 kg (25,353–26,455 lb)
  • Powerplant: 2 × TV3-117VMA-SBM1V turboshaft engines, 1,860 kW (2,490 hp) each
  • Main rotor diameter: 1 main + tail rotor × 16.7–17.3 m (54 ft 9 in – 56 ft 9 in)

Performance

  • Maximum speed: 324 km/h (201 mph, 175 kn)
  • Cruise speed: 310–324 km/h (193–201 mph, 167–175 kn)
  • Range: 520 km (320 mi, 280 nmi)
  • Endurance: 2.75–3 hours
  • Service ceiling: 6,096 m (20,000 ft)

Armament

  • Guns: optional door-mounted machine guns (configurable)
  • Hardpoints: external hardpoints (military configuration optional) , with provisions to carry combinations of:
    • Rockets: 70 mm unguided rockets (Hydra 70 / CRV7 class)
    • Missiles: *UMTAS anti-tank missiles
  • Roketsan Cirit 70 mm guided rockets
  • Air-to-air missiles (e.g. Stinger, Mistral, Bozdoğan, AIM-9) depending on configuration

Avionics

  • Digital glass cockpit
  • Fly-by-wire assisted controls
  • Mission computer architecture
  • Search & rescue radar
  • EO/IR targeting system
  • NVG compatible cockpit

[7]

See also

References

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