Micro-Nano Earth Sensor - SolarWing.space
Product Details

Micro-Nano Earth Sensor

The infrared Earth sensor is an attitude-sensitive device used in satellite attitude control systems.

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Comprehensive specifications and technical information

Micro-Nano Earth Sensor

Quick Overview

The infrared Earth sensor is an attitude-sensitive device used in satellite attitude control systems.

Key Specifications

ParameterValue
ModelC-IRES-LAS-4
Measurement Accuracy0.2° (3σ)
Flight HeritageCompleted qualification
ApplicationLow Earth Orbit satellites
Dimensions (mm)51.5 × 58 × 58
Weight (g)100
Mounting Material2A12 T4
Operating Temperature (°C)−5 to +50
Storage Temperature (°C)−10 to +55
Data Update Rate5 Hz
Communication InterfaceRS-422 / CAN / I²C
Design Life2 years

Key Features

  • Low-cost design and implementation.
  • Integrated opto-electronic structure with high compactness.
  • Lightweight and small form factor.
  • High adaptability to space environments.

Applications

  • Used for attitude determination and control in low-orbit microsatellites and CubeSats.
  • See related products in this series

Documentation & Resources

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Frequently Asked Questions

Common questions about Micro-Nano Earth 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.