Turkish turbine engine and propulsion system design for military aircraft
TRMOTOR designs and develops gas turbine engines and propulsion systems for next-generation military aircraft, wholly owned by Turkish Aerospace Industries. The tech stack—CATIA, NX, ANSYS Fluent, STAR-CCM+, and OpenFOAM—reflects deep embedded simulation and CFD work; the active project list (combustion chamber module design, aero-thermal performance, gas turbine CFD validation) confirms this is an engineering-first, R&D-heavy operation. Hiring is concentrated in senior and mid-level engineering roles, with parallel investment in procurement and contract management—typical of government defense supply chains navigating long tender cycles.
TRMOTOR Güç Sistemleri was founded in 2017 as a wholly owned subsidiary of Turkish Aerospace Industries to advance turbine motor technology and aerospace propulsion capability domestically. The company focuses on design, development, and validation of jet engines and propulsion systems for Turkish military aviation programs. Core technical work spans combustion chamber and afterburner module design, thermal and aerodynamic performance optimization, and full CFD validation workflows. Operations involve subsystem equipment development, tender document management, and cost modeling aligned with defense procurement cycles. The organization is based in Ankara and currently employs 201–500 people.
ANSYS Fluent, STAR-CCM+, and OpenFOAM. CAD work spans CATIA and NX. CFD analysis and model validation are core to active combustion chamber and gas turbine engine projects.
Gas turbine engine and APU projects, including combustion chamber module design, aero-thermal performance improvement, and CFD validation. Active projects also cover subsystem equipment development and tender management for military aircraft programs.
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