Propulsion & Parts Fabricators produces the component layer of the unmanned-aircraft supply chain: piston, turbine and rocket engines, propellers, launchers and catapults, parachute recovery systems, composite airframe sections, antennas, data-link terminals, ground control stations and the smaller fittings that hold an airframe together. Machining, composite lay-up and propulsion test cells run on the same site, and each batch carries material and dimensional inspection records.
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Airborne laser communication can be applied to mobile platforms such as drones and airplanes, and has the advantages of high flexibility, high anti-jamming communication, no electromagnetic radiation, strong confidentiality, and large communication capacity.
The data link system can be applied in different scenarios, and can realize networking between 200km over-the-horizon missile (aircraft) and the ground, as well as between missiles and aircraft,
The data link of telev200 UAV is an integrated mode of data transmission and image transmission, which can realize ground directional antenna tracking, radio positioning, radio ranging, azimuth measurement and MIMO 2 2. The transmission rate can be configured, paired, encrypted and other functions.
The data link of tele V100 UAV is an integrated mode of data transmission and image transmission, which can realize ground directional antenna tracking, radio ranging and MIMO 2 2. The transmission rate can be configured, paired, encrypted and other functions. It has the characteristics of strong an
The integrated data transmission and image transmission mode data link of telev50 UAV can realize ground directional antenna tracking, radio ranging and MIMO 2 2. The transmission rate can be configured, paired, encrypted and other functions. It has the characteristics of strong anti multipath abili
The tele V30 UAV data link is an integrated mode of data transmission and image transmission, which can realize MIMO 2 2. The transmission rate can be configured, paired, encrypted and other functions. It has the characteristics of strong anti multipath ability, light weight, low power consumption,
Teled50 UAV data link is usually used as the data transmission channel of UAV remote control and telemetry. It can realize the functions of self frequency hopping, configurable transmission rate, pairing, encryption and so on. It has the characteristics of strong anti-interference, long transmission
The tele V15 data link is a data transmission and picture transmission integrated mode, which can realize the functions of frequency hopping, diversity reception, configurable transmission rate, pairing and encryption. It has the characteristics of strong anti multipath ability, light weight, low po
The teleD30 data link can be used as the data transmission channel for UAV remote control and telemetry. It can realize the functions of self frequency hopping, configurable transmission rate, pairing, encryption and so on. It has the characteristics of strong anti-interference, long transmission di
1 Provide high quality network transmission
2 Airborne and vehicle ruggedized design
高动态卫星导航接收机可实现多系统组合导航的定位授时功能，满足用户机载、弹载等高速动态应用需求。适用于具有高动态旋转载体的应用。
ZT series small vertical gyro is specially designed for small unmanned aerial vehicle and light missile. It can accurately measure the deviation angle of the aircraft relative to the vertical line, and output the corresponding analog signal for the airborne equipment to record. This series of produc
This product adopts full temperature 0.01 / h high-precision closed-loop optical fiber gyroscope and 20 G high precision quartz accelerometer, pure inertial navigation accuracy lnmile / h (cep50); The product has built-in measurement level multi-mode and multi frequency satellite receiver, and uses
SNC200-IMU is an inertial measurement unit (IMU) based on MEMS technology. It has built-in high-performance MEMS gyroscope and MEMS accelerometer, and outputs 3 angular velocities and 3 accelerations.
SNC200C-IMU MEMS is a domestic inertial measurement unit (IMU) based on MEMS technology. It has built-in high-performance MEMS gyroscope and MEMS accelerometer, and outputs 3 angular velocities and 3 accelerations.
SNC200A-IMU MEMS Inertial Measurement Unit is an inertial measurement unit (IMU) based on MEMS technology. It has built-in high-performance MEMS gyroscope and MEMS accelerometer, and outputs 3 angular velocities and 3 accelerations.
SNC200B-IMU is an inertial measurement unit (IMU) based on MEMS technology. It has built-in high-performance MEMS gyroscope and MEMS accelerometer, and outputs 3 angular velocities and 3 accelerations.
SNC100C-DGI integrated navigation system is composed of MEMS sensors and high-end GNSS receiver board (novatel-718d), which is realized by multi-sensor fusion and navigation algorithm. The product has high reliability and strong environmental adaptability. By matching different software, the product
SNC300C-B0 is a compact inertial navigation system using fiber optic gyroscope (FOG) and micro electro mechanical system (MEMS) accelerometer. It can use external GNSS accurate timing and positioning information for Inertial / satellite integrated navigation. When external GNSS information is invali
SNC300D-DGI is based on cost-effective closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board. It is realized through multi-sensor fusion and navigation solution algorithm to meet the requirements for accurate measurement of attitude, heading and position in application f
SNC500A fiber integrated navigation system is based on high-precision closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board, through multi-sensor fusion and rotation modulation navigation solution algorithm, to provide high-precision attitude, speed and position informat
SNC300A-DGI is based on cost-effective closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board. It is realized through multi-sensor fusion and navigation solution algorithm to meet the requirements for accurate measurement of attitude, heading and position in application f
SNC200A-E inertial navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive external GNSS data, realize multi-sensor fusion and integrated navigation solution algorithm, and has short-term inertial navigation capability when GNSS is invalid.
SNC100C-LITE integrated navigation system has built-in high-performance MEMS gyroscope and accelerometer, which can receive internal GNSS data, realize multi-sensor fusion and integrated navigation solution algorithm, and has short-term inertial navigation ability when GNSS is invalid. The product h
DH-IF3 series three channel high-precision I / F converter adopts the principle of "charge balance", which can continuously measure the input signal without losing information; It has high conversion accuracy, optional signal frequency, low cost and high reliability. It has been applied to vehicle a
DH-G60S series single axis fiber optic gyroscope is an all solid-state medium precision single axis fiber optic gyroscope integrating optics, mechanics and electricity. It follows the classic design concept of traditional fiber optic gyroscope and adopts mature fiber optic gyroscope manufacturing te
DH-G50DA series dual axis fiber optic gyroscope is an all solid state medium precision dual axis fiber optic gyroscope integrating optics, mechanics and electricity. It follows the classic design concept of traditional fiber optic gyroscope and adopts mature fiber optic gyroscope manufacturing techn
DH-G60TA series three-axis fiber optic gyroscope is an all solid-state medium Precision Three-Axis fiber optic gyroscope integrating optics, mechanics and electricity. It follows the classic design concept of traditional fiber optic gyroscope and adopts mature fiber optic gyroscope manufacturing tec
DH-GS OS series single axis fiber optic gyroscope is an all solid-state medium precision single axis fiber optic gyroscope integrating light, machinery and electricity. It follows the classic design concept of traditional fiber optic gyroscope and adopts mature fiber optic gyroscope manufacturing te
DH-G98S series single axis fiber optic gyroscope is an all solid-state high-precision single axis fiber optic gyroscope integrating light, machinery and electricity. It follows the classic design concept of traditional fiber optic gyroscope and adopts mature fiber optic gyroscope manufacturing techn
DH-G120S series single axis fiber optic gyroscope is an all solid-state high-precision single axis fiber optic gyroscope integrating light, machinery and electricity. It follows the classic design concept of traditional fiber optic gyroscope and adopts mature fiber optic gyroscope manufacturing tech
DH-M10 MEMS Gyro assembly integrates high-precision MEMS Gyro (two axes / three axes can be customized), MCU data acquisition and processing system, 422 communication conversion circuit and structural part. Its working principle is that the angular rate and temperature data of MEMS Gyro are transmit
DHN-LM300 series inertial navigation system integrates three-axis high-precision MEMS gyroscope (2 /h), three-axis MEMS accelerometer and corresponding circuit. After the error compensation in the whole temperature range, the navigation level application can be realized. It has the characteristics o
DHN-M050 series inertial navigation system is composed of three-axis integrated optical fiber gyroscope (0.3 / h) newly developed by the company, three-axis quartz flexible accelerometer, power module, high-precision I / F conversion circuit, computer circuit and structural parts. The navigation com
DHN-M060 series inertial navigation system is composed of three-axis 0.3 / h fiber optic gyroscope (gyro diameter 60mm) and three-axis quartz flexible accelerometer, as well as power module, high-precision I / F conversion circuit, computer circuit and structural parts. In the whole temperature rang
DHN-H120 series inertial navigation system is composed of three 0.01 /h fiber optic gyroscopes (gyro diameter 120mm) and three-axis high-precision quartz flexible accelerometer, as well as power module, high-precision I/F conversion circuit, computer circuit and structural parts. The information of
DHN-H90 series inertial navigation system consists of three axis 0.01 /h high-precision prefiber gyroscope and three high-precision quartz flexible accelerometers, as well as a power module, a high-precision 1/F conversion circuit, a computer circuit, a two-axis positioning mechanism. With high "sel
WFDHN-H98 series inertial navigation system consists of high-precision fiber optic gyroscope and high-precision quartz flexible accelerometer, as well as power module, high-precision 1/F conversion circuit, computer circuit and structural parts. The information of odometer and GNSS is fused by kalma
BL-M300 series integrated guidance and control module is composed of flight control solution unit, inertial navigation unit and GNSS receiving unit, which can realize timing control, data management, flight control, inertial /(GNSS navigation calculation; It has the functions of receiving ground con
The telemetry receiver has multi-band, multi-system, multi-channel, high-dynamic telemetry receiving functions, miniaturization, modularization, flexible function configuration, high reliability, strong comprehensive data processing function, integrated uplink spread spectrum modulation transmission
Small fixed wing flight controller (VTOL) is a small flight control system developed for fixed wing VTOL UAV. The flight controller can be applied to 20 ~ 60kg fixed wing UAV. The flight controller has the functions of real-time attitude, position detection, navigation control, task planning and tas
The flight control system of small multi rotor UAV is a compact flight control system developed for multi rotor aircraft. The flight control aircraft has the functions of detection, navigation control, mission planning and mission equipment control, and can control typical four rotor, six rotor, eig
Small UAV flight control system is a compact and reliable flight control system designed for 20 ~ 50kg small UAV system. The flight control system has the functions of attitude and position calculation, flight control, navigation control, mission planning management and mission equipment control.
1 CPU is powered by NXP POWERPC P2020
1 Triplex redundancy CPU structure
1 ZY 8DN01 Double Redundant Flight Control Computer
1 The CPU is powered by NXP POWERPC P1010, with a maximum main frequency of 800MHz
XYFC - 2 XX series of flight control system provide high reliability, high precision navigation and flight control system for fixed-wing drone and following GJB150A and GJB151B reliability standards, it combine digital link system, inertial navigation system, satellite navigation system and multi-se
10KW级小型重油活塞发动机是北京动力机械研究所研制的点燃式二冲程缸内直喷重油活塞发动机，总体采用直列两缸结构布局形式，集成气泵及起发一体电机结构设计，实现整机高紧凑、小迎风面积外形，提高发动机装机适应性，具备空中起动能力,采用轻量化的基于空气辅助的低压燃油雾化技术、高效快速燃烧组织技木等实现发动机快速启动高效稳定燃烧。发动机燃油经济性好、功重比高、技术成熟度高，可适用于各类型小型固定翼无人机，满足燃料安全性的使用要求。
75KW级航空重油活塞发动机是北京动力机械研究所自主研制的点燃式四冲程缸内直喷重油航空活寨发动机。该发动机具有高功重比、长航时、低成本、高升限、重油单一燃料使用的突出特点，采用了智能化高精度电子控制系统、重油高效喷射雾化技术、重油爆震抑制技术、重油高效冷起动系统等多项先进技术，可用于中高空、低速固定翼、旋翼无人飞行器，符合飞行器对单一重油燃料的使用要求。
The low-pressure Air-assisted Direct injection engine system is composed of a two-stroke or four-stroke piston engine and an electronic fuel management control system. The electronic fuel control system is composed of various sensors, actuators, electronic controllers and control software.
The system consists of heavy fuel pressure supply, assisted air pressure supply, pressure relief , fuel metering, fuel gas auxiliary atomization and related pipelines.
The 170cc two-stroke ignition type direct-injection diesel engine is a two-cylinder diesel engine developed based on the application of AADI technology. The engine is widely used in fixed-wing UAV power, rotary-wing UAV extended-range power and portable mobile power power.
Multi fuel enginee 85cc two-stroke ignition type direct injection diesel engine is a single-cylinder diesel engine developed based on the application of AADI technology. It has the characteristics of high power-to-weight ratio, high speed, low fuel consumption, low emission and long life. The engine
The engine has been used in the CH-5 UAV and AR-500B carrier-based unmanned helicopter
ZS12H is a family of two-stroke, two-cylinder horizontally opposed, engines designed for It can be small drones, long-duration drones, forest fire drones, and vertical takeoff and landing drones. , Fixed wings. It has the characteristics of low fuel consumption and high power-to-weight ratio, it s r
The engine has been used in the CH-5 UAV and AR-500B carrier-based unmanned helicopter
300kW military drone heavy fuel engine Main product features：
Custom aircraft engine company was established in 1951 and has more than 70 years of professional engine manufacturing history. Custom aircraft engine company has nearly 2,000 employees. The company is a large enterprise group integrating science, industry and trade. It is China's largest small gene
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
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
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
ZS115发动机： https://www.militarydrones.org.cn/115-horsepower-military-aero-engine-p00269p1.html
ZS20F is a family of two-cylinder, two-stroke, dual-ignition aircraft engines designed for UAV, target drone，powered paragliders, one and two place powered parachutes, single place ultraliht trikes, light single place ultralight aircraft and motor gliders.Mass production of target aircraft and power
ZS115 aero engine is a widely used turbocharged aircraft engine for ultralight and light-sport aircrafts as well as medium altitude long endurance unmanned aerial vehicles. ZS115 offers more performance at high altitude and the best power to weight ratio at better than 1.134 kW/kg.
ZS115HT is a 115 horsepower aviation piston engine. This engine is successfully installed in domestic multiple UAVs and rotorcrafts, it has completed the 8800 meter high altitude flight test, The maximum takeoff height of the engine is 5000 meters, the critical boost height is 7500 meters, and the m
Case：AR500C Altitude unmanned helicopter
Engine take-off power: 350KW
Type: Fixed Pitch Rally Propeller
XH-1870-3 Electric constant speed variable pitch propeller
ZS1870 electric variable pitch propeller is independently developed and designed by our company. It has completed performance test, structural strength test, 400 hour endurance test and flight test. The propeller is made of carbon fiber material, which has the characteristics of high rigidity, high
Electric variable pitch aircraft propeller ZP1900
QHL-750 UAV pneumatic catapult launcher, the latest pneumatic launcher series with renovated three-folded structure and even greater power came up as the ultimate solution for high-altitude long-distance UAV and target drones of up to 750kg.
QHL-150A UAV pneumatic catapult launcher allows takeoff weight of up to 150kg and a maximum 200kg can be realized by its enhanced version, QHL-150B, while both models are towable and compatible for vehicle and vessel use. With high-rigidity structure of longer slide track, QHL-150 medium pressure se
QHL-60 UAV pneumatic catapult launcher is perfect for uav and target drones of takeoff weight under 60 kg and target missile of below 40 kg.
The UAV catapult mainly consists of main frame, lock release mechanism, elastic rope, pulley, shock absorption system, main track pulley, electric winch and other major components. The ejection frame supports fixed-wing UAVs with three-point, three-point, and skid-type layouts, which can be customiz
Elastic power catapult adopts high strength elastic rope as power source, simple operation and maintenance, high cost performance. It can be used for ejection takeoff of 15~25kg fixed wing drone
By using the expansion of the high-pressure gas to do work, the traction of the drone catapult car to obtain a certain speed off the orbit. Compared with the elastic dynamic catapult, it has the characteristics of high ejection stability, good ejection parametric control, high ejection velocity, hig
Trailer type recovery system has the characteristics of high cost performance, simple structure and small storage space. It can quickly operate under the complex terrain of ships, islands and land.
With the purpose of improving the operational mobility of fixed wing UAV, the integrated vehicle ejection and recovery system can realize mobile flight tasks such as rapid response, rapid deployment, withdrawal and rapid transfer in the application fields of border patrol, counter-terrorism and emer
The Mach number range of the transonic wind tunnel test is roughly 0.8~1.4, and the upper limit of the Mach number is mainly limited by the power. The power consumed by the transonic wind tunnel is enormous and increases rapidly with the increase of Mach number. When the Mach number reaches about 1.
A subsonic wind tunnel refers to a wind tunnel with an airflow Mach number ranging from about 0.4 to 0.8 in the test section, and the lower limit of the Mach number can also be as low as 0. The structure of the subsonic wind tunnel is similar to that of the recirculation low-speed wind tunnel, and t
A hypersonic wind tunnel means that the Mach number in the experimental section ranges from about 5 to 14, and the airflow temperature is high enough to prevent liquefaction in the experimental section when the airflow isentropically expanded to the above Mach number, but there is no wind high enoug
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for multi channels of BDS_B1，BDS_B2，GPS_L1 ，GPS_L2 ，GPS_L5，GLONASS_L1，GLONASS_L2，GALILEO L1，GALILEO E5A，QZSS L1，QZSS L2，QZSS L5，IRNSS L5 and IRNSS S frequency signals. It operates on a
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for 4 channels of BDS_B1，BDS_B2，GPS_L1 and GPS_L2 frequency signals. It operates on a power supply voltage of +12V to +32V. It is composed of composed of four main components: antenna a
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for 8 channels of BDS_B1 and GPS_L1 frequency signals. It operates on a power supply voltage of +12V to +32V. It is composed of composed of four main components: antenna array, RF compo
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for 4 channels of BDS_B1, GPS_L1 and GLONASS_L1 frequency signals. It operates on a power supply voltage of +12V to +32V. It is composed of composed of four main components: antenna arr
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for 4 channels of BDS_B1 and GPS_L1 frequency signals. It operates on a power supply voltage of +12V to +32V. It is composed of composed of four main components: antenna array, RF compo
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for 4 channels of BDS_B1, GPS_L1 and GLONASS_L1 frequency signals. It operates on a power supply voltage of +12V to +32V. It is composed of composed of four main components: antenna arr
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for 4 channels of BDS_B1 and GPS_L1 frequency signals. It operates on a power supply voltage of +12V to +32V. It is composed of composed of four main components: antenna array, RF compo
The anti-jamming system is designed to receive, amplify, down-convert, filter, and perform anti-jamming processing for 4 channels of BDS_B1 and GPS_L1 frequency signals. It operates on a power supply voltage of +5V. It is composed of four main components: antenna array, RF component, anti-jamming pr
WF02 Anti-Jam CRPA System supports critical missions by providing jam free GNSS signals. With an 4-array CRPA antenna, the system can assure the normal operation of GNSS receiver in presence of multiple jamming sources. WF-02 Anti-Jam CRPA System can be employed using various configuration and opera
The DFGR-AR05 eight-channel anti-jamming module adopts one anti-jamming processor and connects four two-channel ADs to complete digital down-conversion and anti-jamming signal processing respectively, and can output two channels of DAC digital intermediate frequency or I/Q zero intermediate frequenc
It can be applied to missiles and rockets with a diameter 280mm for attitude control or turning.
Third-party testing of aviation materials in line with international airworthiness standards
Development team lead by a group of very experienced aero-engine specialists.
● Structural analysis and finite element simulation technology
Low-pressure part: 1-stage Fan +Planetary Gear Reducer+2-stage IPC+2-stage LPT
Low-pressure part: 1-stage Fan+2-stage IPC+2-stage LPT
● Low-pressure Shaft: 1 stage Geared FAN + 2 stages IPC + Gear Reducer + 1 stage LPT;
Patented product, compact structure, adaptable to high temperature. It can directly drive the rudder blades, and can also be used for variable flow control of ramjet engines.
BDS/GPS/GLONASS airborne anti-jamming device can simultaneously receive satellite signals of BDS B3, GPS L1 and GLONASS L1 frequency points. The self-adaptive filtering technology points the null direction of the array combining pattern to the direction of the interference, and the beamforming techn
Suitable for missiles or rockets with a projectile diameter greater than or equal to 85mm.
It is suitable for missile or rocket control system whose rotation speed is below 15r/s.
CTF-3 turbofan engine is independently developed by Beijing Power Machinery Institute, China. CTF-3 is a two-spools turbofan engine with a thrust level of 650 kgf. It was designed for small unmanned aerial vehicles (UAV) with high-altitude, long-endurance. The engine has outstanding characteristics
CTF-9 turbofan engine (TRDD-50 A turbofan engine) is an engine with the thrust of 400kg and dual rotors turbofan independently developed by China, which is used for small high-speed UAV. With the outstanding characteristics of high performance and compact structure, the engine is equipped with advan
Rz-21 UAV image transmission data link is composed of airborne antenna, airborne baseband / video compression / RF module, ground antenna and ground baseband / video decompression / RF module. The product has the characteristics of small volume, light weight, small transmission power, long transmiss
Electric variable pitch aircraft propeller ZP1780
FAS-28 advanced small ramjet is a solid fuel ramjet independently developed by Beijing Power Machinery Research Institute. It is composed of inlet, ignition device, charge combustion chamber and supplementary combustion chamber. The engine has the advantages of simple and compact structure, high spe
FG-86 solid rocket motor is a conventional solid rocket motor developed by Beijing Institute of Power Machinery. It consists of front head, combustion chamber, nozzle and igniter. The engine adopts head ignition technology. After ignition, the charge continues to burn and generate rated thrust, and
Light weight, low cost, suitable for missile or rocket control with short working hours.
It is applied to the missile control system to simulate the loading of the steering gear, without generating excess force.
It can be used for simple correction or turning of rotating bombs.
It can be used as an actuator for controlling bullets within 60s.
The icing wind tunnel is a large-scale special wind tunnel with complex performance. It is used to study the icing form, icing tolerance and other characteristics of the windward surface of different components and the external sensing part of the detection instrument when the aircraft is flying und
The controller is integrated with the steering gear, and the integration is high.
It can be used for trajectory correction of rotating projectiles.
LH165DJ-V28 Servo Motor is a product developed to meet the needs of UAV systems for rudder control.
XDCX-03 airborne terminal is an integrated data link radio suitable for small and medium-sized patrol missile groups. It can make air nodes self-organizing and dynamic networking, and meet the typical operational functional requirements of back-end flight control and strike control, node sensor info
The RZ-40 missile aircraft image transmission data link transmits the remote target image monitoring information to the local control center in real time through wireless network transmission technology and relay technology. The operators of the local control center judge the target in real time acc
RZ-70 missile ground image transmission data link is a one-to-one / one-to-two wireless data link transmission system, which includes remote terminal and ground terminal. The remote terminal is composed of missile borne antenna, missile borne video processing module and missile borne baseband / RF m
Technical background Swarm - link is an unmanned aircraft, unmanned systems group of a wireless communication system, is a kind of narrow-band short delays in communication network, has the characteristics of no center and support dynamic topology, has been successfully used in unmanned aerial vehic
The anti-jamming data link system of missile aircraft image transmission is composed of missile borne antenna, missile borne RF module, missile borne baseband / video module, airborne antenna, airborne RF module and airborne baseband / video module. The product transmits the target image monitoring
Suitable for missiles or rockets with a projectile diameter greater than or equal to 85mm.
The rudder blade can be retracted and is suitable for miniature missiles with a projectile diameter of 40mm.
The pneumatic rudder is linked with the gas rudder, and the rudder blades can be retracted.
RZ-31 missile ground image transmission test data link system is composed of missile borne antenna, missile borne baseband / video compression / RF module, ground antenna, ground baseband / video decompression / RF module. The two-way transmission mode of image and data is used to test the performan
The air propeller is a tool that converts the power of the aero engine into the propulsion of the aircraft. The development of the propeller has experienced a process from rise to decline and rise again. Calculation of propeller performance and wind tunnel experiments are the basis for propeller des
Low air consumption, suitable for the control system of missiles with a projectile diameter of more than 200mm.
Purchase shahed 136 drone parts contact: Wechat / Whatsapp： +86 186 8204 2306
It can be applied to occasions with an impact acceleration of 15000g.
The short-range terminal of RZ-90 missile ground image transmission data link compresses the image data of the terminal in real time, encodes and modulates it together with the data information, and sends it to the vehicle / ground terminal in the form of radio wave through the antenna. At the same
It is used in military and civil fields such as small-caliber light missiles, extended-range guided projectiles and fire-extinguishing bombs, including projectile extended-range engines, bottom row devices, small-caliber intelligent ammunition engines and fire-extinguishing bomb boosters. This serie
A supersonic wind tunnel refers to a wind tunnel where the Mach number M of the airflow in the experimental section of the wind tunnel is between 1.4 and 5.
Fast reversing, small size, high efficiency and long working hours.
The controller is integrated with the steering gear, and the sensor adopts a differential transformer, which has high control accuracy. It can be applied to both missiles and unmanned aerial vehicles.
The structure is compact, and 4 servos can be installed in a cabin with a projectile diameter of 122mm.
The controller is integrated with the steering gear, which is suitable for the attitude control of large missiles and UAVs.
The structure is simple, the technology is mature, and there are many applications.
Power must be controlled, suitable for shells or rockets with a speed of 160r/s or more.
The controller is integrated with the steering gear, and the sensor adopts a differential transformer, which has high control accuracy. It can be applied to both missiles and unmanned aerial vehicles.
We customize UAV (including target) rocket boosters according to different needs of customers。
X4 UAV miniaturized thermal imager is a small thermal imager specially designed for UAV. It has the characteristics of light weight, small volume, low power consumption, strong environmental adaptability and simple operation. The lens of the product is designed by optical passive heat difference eli
Unmanned Helicopter Airborne SATCOM ST300
The structure principle is simple and the debugging is convenient.
Compared with the horizontal wind tunnel, the vertical wind tunnel has the advantage that the gravity of the model is parallel to the axis of the test section, which can simplify the balance in the model rotation and the weight component of the rotating part, and is more suitable for the measurement
For details, please download the product manual