PBS is a designer and manufacturer of high-quality aircraft turbojet, turboprop and turbo-shaft engines, which are ideal for unmanned aerial vehicles (UAV’s) and they supply these products throughout the world.
The PBS TJ150 jet engine was developed for unmanned vehicles, training targets and missiles.
Its advantage is its compact design, low weight with a thrust of up to 1,500 N, and low fuel consumption in the given power category. The generator output is 750 W. One of the PBS TJ150 engine versions enables landing on water. The PBS TJ150 engine is a single-shaft jet engine consisting of a radial compressor, radial and axial diffuser, annular combustion chamber, axial turbine and a fixed outlet nozzle.
Standard accessories: included: control system (FADEC), ignition, connecting cable
Optional accessories: electromagnetic fuel valve, fuel filter, control lever, signalling panel, boost pump, reduction valve, converter CAN, converter CAN-USB, user software.
is a 4th-GENERATION turbojet engine. The PBS TJ100 is especially suitable for unmanned aerial vehicles (UAV). These can be used for rescue services, police or reconnaissance purposes and also for other assignments and missions within military applications. These engines are also ideal for gliders and light sports and experimental airplanes. The PBS TJ100 engine is of a compact design and has an excellent power-to-weight ratio of up to 292 lbf (1,300 N) with low fuel consumption for its output category. This engine is also suitable for landing on water.
is a turbojet engine designed for UAV systems, such as target drones and decoy drones, in order to confuse enemy air defenses and small reconnaissance drones. It has the advantage of having a weight of only 7.16 lb (3.25 kg) and a thrust of 88.8 lbf (395 N).
is a turboprop engine especially suited to small aircrafts and unmanned aerial vehicles. These can be used for rescue services, police or reconnaissance purposes and also in agriculture. They can also be used in military applications for other purposes and for Vertical Take-Off and Landing UAVs. The main advantage of this engine is its low weight with a power of 241 HP (180 kW) and its capacity to achieve flight levels of 29,520 ft (9,000 m) with a maximum starting height of 19,680 ft (6,000 m). The system is designed so that the engine can be placed in the aircraft in either pusher or tractor mode.
is a turboshaft engine. This type of engine emerged with the development of modern helicopters. The engine is suitable for smaller and lighter helicopters or for unmanned aerial vehicles. These can be used for rescue services, police or reconnaissance purposes and also in agriculture. The advantage of the engine lies in its small installation dimensions, low weight and high static performance at 241 HP (180 kW) with the capacity to achieve flight levels of up to 29,520 ft (9,000 m) and a maximum starting height of 19,680 ft (6,000 m).
is a small turbojet engine designed for UAV systems, such as target drones and decoy drones, in order to confuse enemy air defenses and small reconnaissance drones. It has the advantage of having a weight of only 4.37 lb (1.98 kg) and a thrust of 47.2 lbf (210 N) It comes with electric starting, a fuel pump and a sparkplug built into the casing of the combustion chamber – the ideal components for UAV systems.