Micro Integrated Electromechanical Solar Array Drive Mechanism - SolarWing.space
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Micro Integrated Electromechanical Solar Array Drive Mechanism

The solar array drive mechanism (SADM) enables satellite solar panels to rotate for sunlight acquisition, tracking, and power optimization.

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Comprehensive specifications and technical information

Micro Integrated Electromechanical Solar Array Drive Mechanism

Quick Overview

The solar array drive mechanism (SADM) enables satellite solar panels to rotate for sunlight acquisition, tracking, and power optimization.

Key Specifications

ParameterValue
ModelC-SADM-4-2A
Transmission Power≥ 1 kW
Flight HeritagePrototype stage
ApplicationMicrosatellite
Dimensions (mm)Ø100 × 160
Weight (g)1200
Mounting MaterialTC4
Operating Temperature (°C)−25 to +65
Storage Temperature (°C)−30 to +70

Key Features

  • Integrated electromechanical structural design.
  • Lightweight and compact form factor.
  • High power-to-volume ratio.

Applications

  • Used for solar array deployment and power transfer in microsatellite platforms requiring efficient and reliable sun-tracking mechanisms.
  • See related products in this series

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Frequently Asked Questions

Common questions about Micro Integrated Electromechanical Solar Array Drive Mechanism

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.