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0 - 100kN turbojet TJ80-120
0 - 100kgfor drone

0 - 100kN turbojet
0 - 100kN turbojet
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Characteristics

Thrust
0 - 100kN
Dry weight
0 - 100kg
Applications
for drone

Description

PBS TJ80-120 is a small sub-sonic jet engine designed for unmanned aerial vehicles (UAVs), including target drones, remote carriers, unmanned combat systems, and other disposable aircraft. Its main advantage is the excellent thrust to weight ratio of 1,200 N at 12.8 kg including accessories. Excellent thrust-to-weight ratio Compact design Built-in BLDC starter-generator including control unit (ECU) and inverter Electric start Quick air-start under 7 seconds Lubrication with fuel mixed with oil, maintenance-free operation The PBS TJ80-120 jet engine is a great example of the continuous development and innovation we aim for in our company. Based on its predecessor, the PBS TJ80-120 jet engine, this engine combines all of the original features together with a significant improvement of the key attributes. We increased the thrust and air mass flow while maintaining the high-quality standard of all PBS products. The maximum measured thrust reached 1,200 N while the engine's weight went up only by 0.7 kg compared to PBS TJ80 900 N at 12.1 kg. The possibilities of ground and in-flight start and restart and saltwater recovery remain unchanged. Furthermore, the engine can be started rather quickly using the windmill starting option. Also, the properties of starting and operating envelopes have not changed. The maximum altitude and speed of the starting envelope remained 6,000 m and 0.6 M, which is satisfactory for air-launched applications. The operating envelope limits stand at 10,000 m altitude and speed of 0.9 M.

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.