Smallsatellite EPS (Power Conditioning & Distribution Unit)
Primary Bus Voltage: 38–46 V
Bus Ripple ≤400 mV
Solar Array Regulation: MPPT, S3R
Static Power: ≤15 W
Output Power: 1000–5000 W
Dimensions: Customizable
MicroSat PCDU
Primary Bus Voltage:21–29 V
Bus Ripple ≤300 mV
Solar Array Regulation: MPPT, S3R
Static Power: ≤12 W
Output Power: 100–1000 W
Dimensions: Customizable
CubeSat PCDU
Primary Bus Voltage:8–12 V
Bus Ripple ≤200 mV
Solar Array Regulation: S3R
Static Power: ≤1.2 W
Output Power: 5–60 W
Size: PC104 format
Weight: ≤200 g
Cubesat Li-ion Battery Pack
Battery Model:18650
Cell Capacity: 3.0 Ah
Cell Voltage: 3–4.2 V
Structure: PC104
Total Capacity: 5–15 Ah
Voltage Range: 8.4–16.8 V
Features: Integrated temperature sensor, heater
MicroSat Li-ion Battery Pack
Battery Model:18650/21700/MP176065 (variable options)
Cell Capacity:3.0 Ah / 5 Ah / 5.6 Ah
Cell Voltage: 3–4.2 V
Structure Options: Standard PC104 board or Aluminum/Magnesium alloy frame
Total Capacity: 15–30 Ah
Voltage Range: 12–48 V
Features: Temperature sensor, heater, high-resistance grounding
Our solar panels use high-efficiency GaAs solar cells and are designed to withstand extreme temperature ranges and long operational lifetimes in orbit.
CubeSat Solar Panel
Solar Cell Efficiency:30% or 32% GaAs
Substrate: PCB Aluminum
Power: Customizable
Operating Temp.: -100°C to +100°C
Lifetime: >3 years
Microsatellite Solar Panel
Solar Cell Efficiency:30% or 32% GaAs
Substrate: CFRP with PI film
Power: Customizable
Operating Temp.: -110°C to +110°C
Lifetime: >5 years
Smallsatellite Solar Panel
Solar Cell Efficiency:30% or 32% GaAs
Substrate: CFRP with PI film
Power: Customizable
Operating Temp.: -130°C to +130°C
Lifetime: >5 years
Our sun sensors offer reliable attitude determination, supporting various field-of-view (FOV) ranges and measurement accuracies, housed in lightweight, durable materials.
Coarse Sun Sensor (Pyramid Type, PASS-90)
FOV:±90°
Dimensions: 55×35×19 mm
Mass: ≤25 g
Housing: Aluminum alloy (natural anodizing)
Operating Temp.: -90°C to +120°C
Analog Four-Quadrant Fine Sun Sensor (SASS-60)
FOV:±60°
Dimensions: 34×21×8 mm
Mass: ≤20 g
Housing: Aluminum alloy (black anodizing/white paint)
Operating Temp.: -90°C to +120°C
Small Digital Sun Sensor (SDSS-60)
FOV:±60°
Measurement Accuracy:0.5° (3σ)
Interface:CAN 2.0B / RS422
Dimensions: 48×36×13.5 mm
Mass: ≤35 g
Housing: Aluminum alloy/white paint
Operating Temp.: -30°C to +70°C
Miniature Digital Sun Sensor (MDSS-60)
FOV:±60°
Measurement Accuracy:0.5° (3σ)
Interface:I2C / UART
Dimensions: 43×14×9.78 mm
Mass:≤8 g
Housing:Aluminum alloy (black anodizing)
Operating Temp.: -30°C to +80°C
Our hinges support solar panel deployment and other mechanical functions, offering lightweight, reliable solutions suitable for CubeSats and microsatellites.
CubeSat Hinge
Mass: < 6.5 g
Size:20×33×7.4 mm
Expand Margin: > 100%
Operating Temp.: -90°C to +100°C
Angle:90°–180° (customizable)
Microsatellite Hinge
Mass: < 60 g
Size:270×51×14.5 mm
Expand Margin: > 100%
Operating Temp.: -90°C to +110°C
Angle: 180° (customizable)
Flexible & Customizable:Dimensions, power outputs, and structural designs tailored to specific mission needs.
High Reliability: Products designed for harsh space environments and long operational lifetimes.
Integrated Solutions: Combine power systems, solar panels, sun sensors, and mechanical components for a complete spacecraft subsystem package.
Global Expertise & Support: Benefit from our extensive experience and responsive customer service, ensuring smooth integration and successful missions.
