Extended-Arm Dual-Axis Solar Array Drive Mechanism - SolarWing.space
Product Details

Extended-Arm Dual-Axis Solar Array Drive Mechanism

Developed for commercial aerospace applications, this long-life, low-cost, and high-reliability drive mechanism features a compact and lightweight structure.

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Comprehensive specifications and technical information

Extended-Arm Dual-Axis Solar Array Drive Mechanism

Quick Overview

Developed for commercial aerospace applications, this long-life, low-cost, and high-reliability drive mechanism features a compact and lightweight structure.

Key Specifications

ParameterValue
ModelC-SADM-3-3B
Output Torque≥ 10 N·m
Flight Heritage2019
ApplicationHongyan / Hongyun Satellite Constellations

Key Features

  • Long service life, low cost, and high reliability.
  • Lightweight and compact design.
  • Adjustable extended arm between dual axes to meet user requirements.

Applications

  • Used in satellite platforms requiring dual-axis solar array tracking and precise positioning, especially in mass-optimized spacecraft configurations.
  • See related products in this series

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Frequently Asked Questions

Common questions about Extended-Arm Dual-Axis 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.