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
Thursday, December 10, 2015TAI and LHTEC Sign Contract for CTS800 Engine
Tuesday, June 16, 2015TAI Selects LHTEC's CTS800 to Power Turkish Light Utility Helicopter

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
CTS800x2
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