Product catalog

Advanced Energy Storage Units for Commercial Rockets and Spacecraft

Our innovative Energy Storage Series offers fully enclosed integrated designs with intelligent data processing, SOC estimation, fault warning, and autonomous temperature control. With a range of voltage platforms, these units meet the diverse power needs of various rocket systems, providing reliable energy solutions for commercial rockets and reusable spacecraft.

High-Temperature Lithium Batteries for Aerospace Applications

Explore our range of high-temperature lithium batteries designed for aerospace use, including long-operating-time, quick-activated, ultra-high-power, and micro lithium batteries. Featuring high efficiency, rapid activation, and wide application across missiles and aircraft systems.

Ni-rich Cathode Materials for Lithium Ion and Sodium Ion Batteries

Explore our range of Ni-rich cathode materials for lithium and sodium ion batteries, featuring high energy density, cost efficiency, and advanced material properties tailored for different applications.

Control Tech Products: Advanced Power Control and Distribution Equipment for Aerospace

Explore our Control Tech Products for spacecraft power management. Featuring a wide BUS voltage range and multiple regulation methods, our equipment provides reliable power distribution for satellites, rockets, and spacecraft. Equipped with intelligent control and modular design, these products ensure stable operation even in extreme environments.

Flexible Solar Wings - High Efficiency Solar Power Solutions

Explore our innovative Flexible Solar Wings, designed for modern space exploration and satellite networking. Featuring two designs, Stacked and Reel-type, these solar wings offer lightweight, high-stored power, and modular capabilities. Ideal for high-efficiency satellite networking, deep space exploration, and lunar bases.

Triple Junction GaAs Solar Cell - High-Efficiency Solar Power for Space Applications

Discover the Triple Junction GaAs Solar Cell - TJ30 CICs, a high-efficiency solar cell assembly designed for advanced space applications. With its superior radiation resistance and impressive efficiency, this solar cell is perfect for satellites, space exploration vehicles, high-altitude UAVs, and more.

High-Efficiency Solar Cell CICs for Space Applications

Explore our High-Efficiency Solar Cell CICs designed for satellite, space station, and deep space applications. Featuring advanced encapsulation technology, these solar cells offer high efficiency, long life, and exceptional radiation resistance.

High-Efficiency Solar Cells for Space Applications

Explore our High-Efficiency Solar Cells designed for satellite, space station, and deep space applications. These cells feature high radiation resistance, thin profiles, and offer outstanding efficiency for demanding aerospace environments.

Near Space Aircraft Energy System - Solar Array & Energy Management

Explore the Near Space Aircraft Energy System designed for altitudes of 20 km to 100 km. Featuring a modular solar array, energy storage, and energy management, this system offers long endurance, low cost, and reliable energy solutions for unmanned airships and aircraft.

Rigid Solar Array for Spacecraft - High Stiffness & Fast Expansion

Discover our Rigid Solar Array, a robust solution for spacecraft energy needs. Featuring high stiffness, rapid expansion, and long service life, this solar array is perfect for CubeSats, SmallSats, and other space vehicles, providing reliable energy supply and wide adaptability.

Solar Arrays for Spacecraft - Comprehensive Solar Power Solutions

Explore our Solar Arrays for spacecraft, including both flexible and rigid solar wings. These solar arrays provide high efficiency, versatile deployment modes, and are tailored to meet the energy demands of next-generation satellites and space vehicles.

Special Solar Panels for Flexible and Portable Energy Solutions

Explore our range of special solar panels, including lightweight folding solar panels and semi-flexible panels for UAVs and vehicles, designed to offer reliable energy in diverse applications.

Cesium Atomic Clocks

Cesium atomic clocks utilize optically-pumping technology to deliver unrivaled frequency accuracy and stability. These high-performance devices are vital for applications such as satellite navigation, power grid synchronization, and precision telecommunications.

TA1000 Optically-pumping Cesium Atomic Clock

Frequency accuracy

≤1E-12

Frequency stability

≤1.2E-11 (1 s)

Frequency reproducibility

≤5E-13

TA1100 Optically-pumping Cesium Atomic Clock

The TA1100 Optically-pumping Cesium Atomic Clock combines advanced optical-pumping technology and laser testing, providing precise frequency standards for communication, power, and transportation systems.

CPT Atomic Clocks

CPT atomic clocks leverage Coherent Population Trapping technology to achieve compact, low-power, and high-stability designs. These advanced timekeeping devices are tailored for modern applications requiring precise timing, including satellite navigation, underwater systems, and communication networks.

XHTF1025-S CPT Atomic Clock

XHTF1025-S CPT Atomic Clock: 10 MHz single output, compact (86×86×42 mm), high frequency accuracy, low power consumption.

XHTF1040 CPT Atomic Clock

The XHTF1040 CPT Atomic Clock features ultra-low power consumption, miniature structure, and comprehensive timing capabilities including 1PPS synchronization and TOD output.

XHTF1040B CPT Atomic Clock

The XHTF1040B CPT Atomic Clock features miniature design, low power consumption, and advanced timing capabilities with TOD short message output, suitable for high dynamic situations.

Rubidium Atomic Clocks

Rubidium atomic clocks are high-performance, compact, and low-power-consumption devices delivering precise 10 MHz outputs. They are widely used in aerospace, defense, communication, and other high-reliability applications.

XHTF1003-C1 Rubidium Frequency Standard

The XHTF1003-C1 is a high-performance rubidium frequency standard featuring excellent phase noise characteristics, compatible with LPRO Rb atomic clock, and offering RS-232C communication capabilities.

XHTF1003-H Rubidium Frequency Standard

The XHTF1003-H is a high-performance rubidium frequency standard featuring excellent phase noise characteristics, compatible with LPRO Rb atomic clock, and offering RS-232C communication capabilities.

XHTF1011 Rubidium Frequency Standard

The XHTF1011 High Accuracy Rubidium Oscillator delivers wide-temperature operation from -40°C to +70°C with selectable stability, phase-noise, and temperature options, fast 1PPS disciplining, and RS-232C control for airborne, vehicular, and shipborne time-frequency systems.

XHTF1012LN Low Phase Rubidium Atomic Clock

The XHTF1012LN Low Phase Rubidium Atomic Clock offers ultra-low phase noise and high short-term frequency stability, making it ideal for precision applications in radar, communication systems, and scientific research.

XHTF1021 Compact Rubidium Atomic Clock

The XHTF1021 Compact Rubidium Atomic Clock offers precise timing and synchronization with low power consumption, making it suitable for aerospace, aviation, navigation, and communication industries.

XHTF1022C Ultra-thin Rubidium Atomic Clock

The XHTF1022C Ultra-thin Rubidium Atomic Clock offers precise timing, low power consumption, and compact design, making it ideal for critical applications in aerospace, navigation, and power systems.

XHTF1031R Miniature Rb Atomic Clock

The XHTF1031R is a miniature rubidium atomic clock featuring low power consumption, compact structure, and compatibility with SA.3 series atomic clock, ideal for aviation and aerospace applications.

Space-borne Rb Atomic Clock (Custom)

High-precision space-borne rubidium atomic clock designed for navigation satellites, communication satellites, and space stations, featuring exceptional frequency stability and radiation resistance.

A1013Q Universal Four-Port Chip

Process Technology

0.13 μm

Dimensions (mm)

28 × 28 × 7

Weight (g)

12

Microsatellite Integrated Electronics

Model

C-ICDE-DMR/C-2

Technology

SiP / SoC

Flight Record

First flight in 2019

NASSAT Computer

Model

C-GNCC-S-1

Technology

SiP / SoC

Flight Record

First flight in 2015

NASSAT Dual-Module Computer

Model

C-GNCC-DMR/C-7

Technology

SiP / SoC

Flight Record

First flight in 2018

Quad-Core SoC2012 32-bit Space Application On-Chip System

Process Technology

0.13 μm

Dimensions (mm)

37 × 37 × 3

Weight (g)

12

SiP2113 Universal Onboard Computer Module

Function

Computing module functionality

Packaging Technology

Bare-die based packaging

Dimensions (mm)

35 × 35 × 2

SiP2115 Universal Onboard Computer Module

Function

Computing module functionality

Packaging Technology

Bare-die based packaging

Dimensions (mm)

37 × 37 × 5

SiP6117M Programmable Signal Processing Module

Function

Programmable signal processing SiP

Packaging Technology

Bare-die based packaging

Dimensions (mm)

22 × 22 × 2

SoC2008 32-bit Space Application On-Chip System

Advanced spacecraft component for satellite systems.

SoC2016 32-bit Space Application On-Chip System

Process Technology

0.13 μm

Dimensions (mm)

41 × 41 × 10

Weight (g)

12

SpaceOS Embedded Real-Time Operating System

Scheduling Algorithm

Priority-based fixed preemptive scheduling with time-slice round-robin support for tasks of the same priority

Supported CPU Architectures

SPARC and ARM

Supported Number of Tasks

Unlimited

The Core Components of the Micro-Satellite Controller

A series of highly integrated and miniaturized electronic system chips have been developed for micro- and nanosatellite control applications. These include the SoC2008 32-bit onboard application system chip, which has already been widely adopted in satellite electronic systems, and the SoC2012 32-bit onboard application system chip, designed for general onboard computing and attitude control with radiation tolerance up to 300 krad and a processing performance of 300 MIPS @ 100 MHz. The series also includes SoC2016 (LEON4 + DSP), SiP2113 general-purpose onboard computer module, and SiP2214 general-purpose onboard computing module with integrated data management functions. The SiP2115 general-purpose onboard computing module incorporates the A1013Q chip and serves as a typical onboard computer module for micro- and nanosatellites.

XY28F256KLV (3.3V) 32K×8bit Anti-Radiation PROM

Process Technology

0.13 μm

Dimensions (mm)

17.8 × 12.5 × 2.5

Weight (g)

2.1

XY28F256KV (5V) 32K×8bit Anti-Radiation PROM

Process Technology

0.13 μm

Dimensions (mm)

17.8 × 12.5 × 2.5

Weight (g)

2.1

XY50601 Radiation-Resistant Synchronous Rectifier Buck Switching Power Chip

Function

Switching Power Supply

Process Technology

0.18 μm

Dimensions (mm)

12.7 × 7.4 × 2.2

XY61580 Radiation-Resistant 1553B Bus Controller

Process Technology

0.5 μm

Dimensions (mm)

48 × 26

Weight (g)

< 15

XY6664RH Radiation-Resistant 8K×8bit PROM

Process Technology

0.18 μm

Dimensions (mm)

35.5 × 15.5 × 3

Weight (g)

4.7

XY8R512K40/1M40 20M/40Mb Anti-Radiation SRAM

Process Technology

0.13 μm

Dimensions (mm)

29 × 29 × 3

Capacity

512 K / 1 M × 40 bit

090 Digital Reaction Wheel

Model

C-SRWMI-090-0.1A

Rated Momentum

0.12 N·m·s

Flight Heritage

First flight in 2016

130 Standard Reaction Wheel

Model

C-GRWMI-130-0.5A

Rated Momentum

0.5 N·m·s

Flight Heritage

First flight in 2012

160 Digital Reaction Wheel

Model

C-SRWMI-160-4A

Rated Momentum

4 N·m·s

Flight Heritage

First flight in 2015

5 N·m·s Variable-Speed Control Moment Gyroscope (VSCMG)

Model

C-CMG-5/5-A

Rated Momentum

0.5 N·m·s

Flight Heritage

First flight in 2012

Extended-Arm Dual-Axis Solar Array Drive Mechanism

Model

C-SADM-3-3B

Output Torque

≥ 10 N·m

Flight Heritage

2019

Metal Coriolis Vibratory Gyroscope (CVG)

Dimensions (mm)

B110 × L110 × H90

Weight (g)

1000

Power Consumption

≤ 6 W

Micro Dual-Axis Antenna Drive Mechanism

Model

C-GDAM/A-11-3A

Output Torque

> 3 N·m

Flight Heritage

2019

Micro Flywheel Combination

Model

C-AOFW-3-1A

Rated Momentum

60 mN·m·s

Flight Heritage

Completed in 2017

Micro Inertial Attitude Sensor

Model

C-IAS-M-EMS-4

Measurement Accuracy

< 3.3°/h

Flight Heritage

First flight in 2015

Micro Integrated Electromechanical Solar Array Drive Mechanism

Model

C-SADM-4-2A

Transmission Power

≥ 1 kW

Flight Heritage

Prototype stage

Micro Magnetic Torquer

Model

C-GMAT-0.5 / C-GMAT-1 / C-GMAT-10 / CGMAT(I)-10

Magnetic Moment

0.5 A·m² / 1 A·m² / 10 A·m²

Flight Heritage

2015–2019 (multiple flight missions)

Micro-Nano Flywheel and Magnetic Torquer Assembly

Model

C-AOWM-3-3-1A

Rated Torque

0.4 mN·m·s

Flight Heritage

Completed in 2015

0.1 MPa Micro Pressure Sensor

Dimensions (mm)

22 × 22 × 56

Mass (g)

≤ 50

Mounting Material

1Cr18Ni9Ti

0.2 N Single-Component Thruster Assembly

Dimensions (mm)

Φ48 × 92

Mass (g)

175 ± 10

Propellant

Hydrazine

1 N Single-Component Thruster Assembly

Dimensions (mm)

Φ58 × 128

Mass (g)

300 ± 20

Propellant

Hydrazine

1 to 15 mN Electromagnetic Ratio Cold-Gas Thruster

Dimensions (mm)

Φ21 × Φ21 × 48

Mass (g)

≤ 40

Mounting Material

1Cr18Ni9Ti

2 MPa Micro Pressure Sensor

Dimensions (mm)

26 × 26 × 62

Mass (g)

60

Mounting Material

316L

ADN-Based Non-Toxic Thruster Series

The ADN-Based Non-Toxic Thruster Series includes thrusters ranging from 0.2 N to 20 N, designed to provide high-performance and environmentally friendly propulsion solutions. Two ADN-based monopropellant formulations were developed: a medium-energy propellant with a theoretical specific impulse of approximately 220 s, and a high-energy propellant reaching up to 245 s. Catalyst optimization further enhances combustion efficiency and propellant compatibility.

ADN-Based Single-Component Micro-Propulsion Module

Dimensions (mm)

110 × 100 × 94

Mass (g)

1300

Total Impulse

800 N·s

Butane Micropropulsion Module

Dimensions (mm)

100 × 100 × 100

Mass (g)

900

Total Impulse

200 N·s

C-GLV-3 Self-Locking Valve

Dimensions (mm)

Φ31 × 174 × 53

Mass (g)

350 ± 10

Design Life

8 years

Integrated Propulsion Structure Module

Dimensions (mm)

350 × 386 × 490

Dry Mass (kg)

7.1

Propellant

HAN-Based Green Propellant

Low-Power Hall Thruster

power_et_h300_1

300 W

power_et_h600_1

600 W

dimensions_et_h300_1

144 × 114 × 91 mm

MEMS Solid Micro-Thruster Array

Dimensions (mm)

70 × 70 × 30

Mass (g)

200

Impulse Range

10⁵–10⁶ N·s

Micro Cathode Arc Propulsion Module

Dimensions (mm)

100 × 100 × 40

Mass (g)

600 ± 50

Propellant

Titanium / Tungsten

Micro-Nano Satellite Position Control Integrated Module

Dimensions (mm)

280 × 250 × 400

Dry Mass (kg)

1.8

Propellant

HAN-Based Green Propellant

Micro-Newton Variable Thrust Module

Dimensions (mm)

205 × 80 × 80

Mass (kg)

≤ 0.4

Mounting Material

TC4 (Titanium Alloy)

Single-Component 30 μm Mesh Filter

Dimensions (mm)

130 × 20 × 20

Mounting Material

316L Stainless Steel

Operating Temperature (°C)

+5 to +60

Single-Set Element Gas/Liquid-Filling Valve

Dimensions (mm)

90 × 32 × 42 (C-GFDV–1/2) / 71 × 32 × 42 (C-GFDV–1A/2A)

Mounting Material

316L Stainless Steel

Operating Temperature (°C)

+5 to +60

Small Satellite Positional Orbit Control Propulsion Module

Dry Mass (kg)

5.7

Propellant

HAN / ADN

Operating Temperature (°C)

0–50

Solid Cold-Gas Micropropulsion Module

Dimensions (mm)

96 × 96 × 98

Mass (g)

1200

Total Impulse

80 N·s

Tiny Satellite Position-Controlled Propulsion Module

Dimensions (mm)

600 × 400 × 400

Dry Mass (kg)

3.6

Propellant

ADN

Tiny Ultra-High-Pressure Cold-Gas Propulsion System

Dimensions (mm)

190 × 430 × 190

System Mass (kg)

≤ 2

Total Impulse

> 700 N·s

Commercial Integrated Digital Solar Sensor

Model

C-SS-APS-Img/P-2

Measurement Accuracy

≤ 0.05° (3σ)

Flight Heritage

Completed qualification

Dual-Axis Micro Analog Solar Sensor

Model

C-SS-SiC-Ana/B-2B

Measurement Accuracy

< 0.5°

Flight Heritage

First flight in 2015

High-Dynamic Nano Star Sensor

Dimensions (mm)

50 × 50 × 89.4

Weight (g)

260

Mounting Material

2A12 T4

Long-Life Micro Star Sensor

Model

C-ST-HA-APS7-1

Measurement Accuracy

5″ (3σ)

Flight Heritage

Completed qualification

Long-Life Nano Star Sensor

Model

C-ST-MA-ASP1-1D

Measurement Accuracy

5″ (3σ)

Flight Heritage

Completed qualification

Micro-Nano Earth Sensor

Model

C-IRES-LAS-4

Measurement Accuracy

0.2° (3σ)

Flight Heritage

Completed qualification

Micro Star Sensor

Model

C-ST-MA-APS4-1

Measurement Accuracy

3″ (3σ)

Flight Heritage

First flight in 2016

Monolithic Solar Sensor

Model

C-SS-SiC-ANA/B-2B

Measurement Accuracy

0.05° (3σ)

Flight Heritage

Completed qualification

Nano Star Sensor

Model

C-ST-MA-APS1-1A

Measurement Accuracy

10″

Flight Heritage

First flight in 2017

Split-Type Micro Star Sensor

Model

C-ST-HA-APS6-1

Measurement Accuracy

3″ (3σ)

Flight Heritage

Completed qualification

Ultra-Compact Star Sensor

Measurement accuracy

30″ (3σ)

Data update rate

5 Hz

Dynamic performance

1°/s