TLUH Initial Operational Capability (IOC): 2020 Total Production: ? Also Known As:Turkish Light Utility Helicopter Origin:Turkey Corporations: Turkish Aerospace Industries
Parent System:TLUH Initial Operational Capability (IOC): 2020 Total Production: ?
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Description: The Turkish Light Utility Helicopter (TLUH) is a 5-ton class twin-engine, tactical helicopter developed by Turkish Aerospace Industries (TAI) to meet the requirements of the Turkish military. The new helicopter is expected to be certified by EASA by 2020. TAI selected the LHTEC CTS800 engine to power the new helicopter at the Paris Air Show on June 16, 2015.
TLUH Specifications
Number of Engines: 2 Weight Max Takeoff Weight: 5,000 kilogram (11,023 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)
TLUH News
There are 2 news between 16 Jun 2015 and 10 Dec 2015