X
TEI'Yİ SOSYAL MEDYADA<BR>TAKİP EDİN
ARAMAK İSTEDİĞİNİZ<BR>KELİMEYİ YAZINIZ
LÜTFEN WEB SİTESİNİN<BR>DİLİNİ SEÇİNİZ
TR
EN
TJ35 TURBOJET ENGINE

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. TJ35 turbojet engine have been developed as part of these studies.

 

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.

 

Main characteristics and technical specifications of the TJ35 engine:

  • Air and propane start
  • ECU with ground station data link

Max. Thrust (N)/(lbf)

178/40

Specific Fuel Consumption (kg/N.h)/(lb/lbf.h)

0.135/1.35

Max. Rotor Speed (RPM)

120,000

Dry Weight (kg)/(lb)

3.1/6.8

Length (mm)/(in)

250/9.8

Diameter (mm)/(in)

130/5.1

Time Between Overhaul (h)

25+

 

All values are based on ISA at sea level conditions.