TM TJ-1000 Turbojet

The TJ-1000 is a single spool turbojet engine capable of providing up to 1100 LBF of thrust. A very affordable choice for high performance UAVs, cruise missiles and air target drones. The large number of applications for this engine makes it very attractive and a key item within military aeronautical industries. It is currently being used as the main propulsion system of the AVTM300 Brazil cruise missile.

GENERAL CHARACTERISTICS

• Type: Single spool turbojet

• Length: 1180 mm

• Diameter: 350 mm

• Dry weight: 70 kg

• Maximum uninstalled thrust: 4.44 kN @SSL (1100 lbf)

• Specific fuel consumption: 1.16 kg/kgf/hr

 COMPONENTS

• Compressor: 4 axial stages

• Combustor: Annular

• Turbine: Single axial stage