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The CTJ-1 turbojet engine is a 1100N thrust level turbojet engine with a wide working range. It is mainly composed of a single-stage centrifugal compressor, a baffled annular combustion chamber and a single-stage axial-flow turbine. It uses a digital electronic control unit to supply oil for the eng
This is a micro turbojet engine specially developed for target drones and small tactical missiles.
Compressor: 3-stage axial flow, the supercharging ratio is 3.8, of which the first-stage compressor is a titanium alloy integral blade rotor (IBR).
Basic parameters of 180KG thrust turbojet engine
The NM-150P turbojet engine is a small turbojet engine composed of a single-stage centrifugal compressor and an axial flow turbine, with a maximum net thrust of 150daN. The engine runs stably and reliably, and can provide power for high-subsonic UAVs, unmanned target drones, small missiles and other
The NM-40 turbojet engine is a single-shaft small jet engine with a centrifugal compressor and a centripetal turbine, with a maximum static thrust of 40kg. The engine adopts a mixed fuel system design, and the engine control unit (ECU) adopts a digital fuel adjustment design, which can monitor and p
TWP100E 100kg thrust turbojet engine is a low-cost, short-life, high thrust-to-weight ratio small turbojet engine independently developed by the Chinese Academy of Sciences.
Nm-80wp turbojet engine is a turbojet engine composed of a single stage centrifugal compressor and an axial flow turbine, which has strong anti-overload and distortion ability. It has three starting modes: motor driven rotation, air blowing and gunpowder impact. At present, it is used in large mobil
This 200 kg thrust turbojet engine is used in aircraft such as drones, target drones and missiles, and is made in China. Stable and reliable performance, high cost performance, Custom built to customer specifications.
Technical Specifications for 6.4kg Micro Turbojet Engine
Technical Specifications for 2kg Thrust Jet Engine
Gas turbine engine is an essential power plant in modern day high speed UAS (Unmanned Aerial System) for various applications
The SXH-1200N 80kg thrust turbojet engine is a small turbojet engine with low cost, high thrust-to-weight ratio and high reliability independently developed by Feihang Power Technology Co., Ltd. The overall structure of single-stage centrifugal compressor + short annular downstream combustion chambe
Single shaft compact structure design
Single shaft compact structure design
Turbojet Engine for target drone QH-WP100A
With high reliability and low cost, it can be used in the flight power system of various high-performance UAVs, target missiles, cruise missiles and other military and civilian products.
Small size, light weight, thrust weight ratio of more than 10, integrated combustion and sliding, one key start, suitable for target aircraft, target bombs, individual aircraft and other flight platforms.
DLE engines from China. DLE engine China was established more than ten years, independent research and development production of DLE series engine, products with excellent performance, is the only Chinese-made engine into the international race, won the domestic and foreign users of the widely accla
Limbach L550E is a four-cylinder, two-stroke, horizontally opposed engine, with excellent performance, outstanding reliability and excellent power-to-weight ratio, which has been used in many fixed-wing unmanned stages in France, South Africa, Thailand, Singapore and domestic Chinese Academy of Scie
100kW级电喷航空活塞发动机是北京动力机械研究所在高增压技术优势上进行的创新研究，保持了发动机原有的高工作升限，提高了发动机的功率输出，同时采用电喷系统在保持发动机工作可靠性的前提下，降低发动机油耗，为各型高空飞行器及通航飞机提供优质的动力选择。
The MDR 208 engine is specially designed and developed for medium and large unmanned aerial vehicles. Compared with the traditional AR731/741 rotary engine, its combustion chamber is designed with ceramic plating, which not only prolongs the service life and reliability, but also greatly reduces the