Dual-Axis Micro Analog Solar Sensor - SolarWing.space
Product Details

Dual-Axis Micro Analog Solar Sensor

The dual-axis micro analog solar sensor uses four silicon photodiodes as the sensing elements to measure the solar incident angle in two axes.

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Comprehensive specifications and technical information

Dual-Axis Micro Analog Solar Sensor

Quick Overview

The dual-axis micro analog solar sensor uses four silicon photodiodes as the sensing elements to measure the solar incident angle in two axes.

Key Specifications

ParameterValue
ModelC-SS-SiC-Ana/B-2B
Measurement Accuracy< 0.5°
Flight HeritageFirst flight in 2015
ApplicationMicrosatellite
Dimensions (mm)40 × 34.5 × 13.5
Weight (g)37
Mounting MaterialLY12 BCZYu
Operating Temperature (°C)−100 to +90
Storage Temperature (°C)−105 to +105
Communication InterfaceAnalog current signal output

Key Features

  • Low cost and high reliability.
  • Lightweight and compact design.
  • Wide operating temperature range and strong radiation resistance.

Applications

  • Used in microsatellite systems for sun vector measurement and solar array attitude detection.
  • See related products in this series

Documentation & Resources

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Frequently Asked Questions

Common questions about Dual-Axis Micro Analog Solar Sensor

What spacecraft platforms is this system compatible with?

This system is compatible with microsatellites, nanosatellites, CubeSats, and larger spacecraft platforms. It features modular design with standard interfaces for easy integration into various mission architectures and supports both commercial and scientific applications.

How does this system enhance spacecraft capabilities?

The system provides advanced functionality with reduced size, weight, and power consumption. It offers improved reliability through redundancy, radiation tolerance, and proven space-qualified components with extensive flight heritage.

What are the key performance specifications?

Key specifications include low power consumption, wide operating temperature range, high radiation tolerance (TID >100 krad), compact form factor, and long operational lifetime (>10 years). The system meets all relevant space qualification standards.

How is system integration and testing performed?

We provide comprehensive integration support including detailed interface specifications, test procedures, and simulation tools. All systems undergo thorough environmental testing, functional verification, and compatibility validation before delivery.

What documentation and support is available?

Complete technical documentation includes user manuals, interface control documents, test reports, and application notes. Our engineering team provides integration support, training, and ongoing technical assistance throughout the mission lifecycle.