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Additional information

Airframe: Eurocopter Tiger HAD/E, HAD/F, UHT
Output Shaft Power: 1094 kw (Top)1322 kw (SUP)1000 kw (MCP)
Customer: OCCAR (FR, GE, SP)

ITP responsibility

Oil Cooling System (OCS)
Manufacturing of air intake, compressor casing, first stage radial stator and second stage diffuser
Design of the power turbine (PT) and the inter turbine duct (ITD)
Manufacturing of the PT discs and casing, and of the ITD

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