Its advantage is its low weight of 3.8 kg and thrust of 395 N. The PBS TJ40-G2 jet engine is a single-shaft turbine small jet engine with a one-stage radial compressor, radial and axial diffuser, annular combustion chamber, one-stage axial turbine and outlet nozzle. The generator output is 200 W, and with an external converter it is an additional 900 W.

Standard accessories: fuel pump and filter, engine control unit (ECU), connecting cables, fuel hose, data terminal, battery (4s Li-Fe - 2,5 Ah), CAN connector

Compact design - all accessories incorporated in the engine (except for the fuel pump)
Excellent thrust-to-weight ratio, low power consumption in the given power category
Easy and fast start
Repeatable start on the ground and in flight
Any engine position during start
Shortened start sequence under 25 seconds

Technical parameters

Max. thrust: 395 N / 89 lbf
Outer diameter: 147 mm / 5.79 in
Length: 373 mm / 14.69 in
Weight: 3.8 kg / 8.38 lb