Airplane Engines

PBS AEROSPACE production division, is a manufacturer and developer of aircraft turbo jet, turboprop and turbo-shaft engines. During development, PBS AEROSPACE focused on smaller turbine engines used mainly in smaller and experimental aircraft, helicopters and unmanned aerial vehicles. PBS engines hold an advantage in that they can be used for all these categories. Due to their high-level parameters, PBS engines hold a major advantage with their lightweight structure and weight-to-power ratio ranking them among world leaders in their field. PBS AEROSPACE Inc. (US) is the supplier of these engines in the USA.

PBS TJ100

is a 4th-GENERATION turbojet engine. The PBS TJ100 is especially suitable for target drones, manned and other unmanned vehicles (UAVs). These can be used for rescue services, police or reconnaissance purposes and also for other assignments. 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 (1,250 N) with low fuel consumption for its output category. This engine is also suitable for landing on water.

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PBS TP100

is a turboprop engine especially suited to unmanned aerial vehicles and small aircrafts. 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.

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PBS TS100

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).

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