PBS TJ40-G2

PBS.TopImage.Btn.Scroll

Jet Engine PBS TJ40-G2

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.

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

Standard accessories: fuel pump and filter, engine control unit (ECU), connecting cables, fuel hose, data terminal, CAN connector

Technical parameters

Technical parameters	Metric units	Imperial units
Max. thrust	425 N	96 lbf
Outer diameter	147 mm	5.79 in
Length	304 mm	11.97 in
Weight	3.8 kg	8.38 lb

Key parameters

Pyrotechnic ignition - under development

The engine allows to start in seconds

Salt water recovery - under development

The engine allows reuse after landing in salt water

Ground and In-Flight Restarting

The engine's ability to start in any position and short startup sequence of under 25 seconds characterize this small jet engine developed especially for unmanned applications.

Output power of 900 W for the aircraft's needs

The generator output is 200 W, and with an external converter it can deliver another 900 W of power.

Service, spare parts and overhauls of aerospace technology

We provide service of the highest quality for all users of our aerospace technology products.

We have long been working to extend the service life of our products, e.g. by introducing new technologies to produce the most exposed parts. Our turbine-based aircraft equipment regularly receives very good references.

More information