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TEI-TJ35
Turbojet Engine

TEI TJ35 Header

TEI develops turbojet and turboprop engines to meet the gas turbine need of competitive, innovative, high-tech Unmanned Aerial Vehicles (UAV) which are anticipated to be released to the domestic market first and to the international market in the long-term.

Accordingly, R&D studies continue at TEI since 2004. In consequence of these activities, TJ35 turbojet engine has been developed.

Main characteristics and technical specifications of the TJ35 engine:

Air-start and propane start
ERU featuring data connection with ground station
Maximum thrust: 178/40 (N/lbf)
Specific Fuel Consumption (kg/N.h)/(lb/lbf.h): 0.135/1.35
Maximum Shaft Speed: 120,000 RPM
Dry Weight: 3.1/6.8 (kg/lb)
Length: 250/9.8 (mm/in)
Diameter: 130/5.1 (mm/in)
Maintenance Interval: 25+ (h)

All values are relative to sea level under ISA conditions.

TJ35 Turbojet Engine

Increasing demand for unmanned aerial vehicles, and therefore development of projects in this direction in the military and civil aviation industries in Turkey have raised the needs regarding the thrust systems of aircraft. Accordingly, TJ35 turbojet engine development project was realized between 2004-2005 with the aim of technical capability development.

TEI TJ35 Motor