Turbojet engine BPS TJ200

The BPS-TJ200 turbojet engine is a low-cost, short-life, high thrust-to-weight ratio small turbojet engine independently developed by Shandong Earth Shield Defense Technology Co., Ltd..

Each engine undergoes a series of verification tests and acceptance tests before leaving the factory, and its performance indicators meet the requirements of the acceptance test outline.

he engine mainly consists of a 1-stage high-pressure ratio centrifugal compressor, an annular evaporation tube combustion chamber, a 1-stage axial flow turbine, a casing, and a fuel regulation system. The engine adopts a unique high hub-to-tip ratio compressor design and, through an embedded generator mounting structure, achieves 1700W power extraction from the engine itself..

Technical parameters

	Metric units	Imperial units
Max. thrust	1,900 N	423.75 Ibf
Weight	≤ 25 kg	≤ 55.11 lb
Outer diameter	320 mm	12.59 in
Lenght	645 mm	25.39 in
Max. speed( (r/min)	45,000	45,000

Leaflet

Typical applications

The ES-BPS-TJ200 turbojet engine are ideal for a variety of applications, including missiles and target drones, where they are particularly valued for the saltwater recovery capability. Their compact design and low weight make them a perfect fit for high-speed UAV and UCAV systems. The engines are also suitable for remote carriers.