CTF-9 Turbofan Engine（400kgf）(TRDD-50 A Turbofan Engine)

Vue d'ensemble

CTF-9 turbofan engine (TRDD-50 A turbofan engine) is an engine with the thrust of 400kg and dual rotors turbofan independently developed by China, which is used for small high-speed UAV. With the outstanding characteristics of high performance and compact structure, the engine is equipped with advanced electrical, control and health management, and can meet the power needs of small UAV with high elevation and large range. Main performance indicators Flying Mach number: 0~0.9 Maximum take-off thrust of engine: 400kgf (H=0, Ma=0, ISA) Engine fuel rate: 0.65kg/ (kgf. h) (H=0, Ma=0, 1SA) Engine inlet diameter/outer diameter: 279mm/330mm Weight: 82kg (body net weight) Cycle of the first restoration :500h Power supply capacity :8kW

Spécifications techniques

Caractéristiques principales : Ceiling 12.5km, Flying Mach number 0~0.9, Maximum take-off thrust of engine 400kgf (H=0, Ma=0, ISA), Engine fuel rate 0.65kg/ (kgf. h) (H=0, Ma=0, 1SA), Engine inlet diameter/outer diameter 279mm/330mm, Engine length 855mm, Weight 82kg (body net weight), Cycle of the first restoration 500h, Power supply capacity 8kW.

Spécifications techniques

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