The PBS TJ100 is a 4th-GENERATION turbojet engine. The PBS TJ100 is perfectly suited for UAVs and UCAVs applications. The PBS TJ100 engine is of a compact design and has an excellent power-to-weight ratio of up to 281 lbf with low fuel consumption for its output category. This engine is also suitable for landing on water.
Main features
- Compact design, excellent thrust-to-weight ratio and low fuel consumption for its category.
- The integrated starter-generator ensures reliable 24V battery start-up, supplies electricity to the vehicle’s onboard wiring and cools the engine after shutdown.
- Classic design – radial compressor and annular combustion chamber, axial turbine and fixed output nozzle.
- Standard equipment fuel-oil system, control system, ignition unit, connection cables and manual or fully automatic control.
- Lower operational and starting speed of the base model.