Microturbo TRI 60

Microturbo TRI-60
Type	Single Spool Turbojet
National origin	France
Manufacturer	Microturbo
First run	6 June 1974.
Major applications	Storm Shadow / SCALP EG ; RBS-15
Variants	Microturbo TRI-40

The Microturbo TRI 60 is a small, expendable turbojet engine developed for use in cruise missiles, target drones, and other small unmanned air vehicles. Variants of this engine produce from 3.5 to 5.3 kN (790 to 1,190 lbf) of thrust. The engine first ran in 1974.

^ RIDEAU, Jean-François, GUYADER, Gilles, CLOAREC, Alain (2008). MICROTURBO Families of Turbojet Engine for Missiles and UAV's From the TR60 to the new bypass turbojet engine generation. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 21–23 July 2008, Hartford, Connecticut. AIAA 2008-4590.

[aiaa-1] RIDEAU, Jean-François, GUYADER, Gilles, CLOAREC, Alain (2008). MICROTURBO Families of Turbojet Engine for Missiles and UAV's From the TR60 to the new bypass turbojet engine generation. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 21–23 July 2008, Hartford, Connecticut. AIAA 2008-4590.

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