Micro Dual-Axis Antenna Drive Mechanism - SolarWing.space
Product Details

Micro Dual-Axis Antenna Drive Mechanism

The CE-5 series micro dual-axis antenna drive mechanism is designed to control antenna orientation for ground communication and data transmission.

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Comprehensive specifications and technical information

Micro Dual-Axis Antenna Drive Mechanism

Quick Overview

The CE-5 series micro dual-axis antenna drive mechanism is designed to control antenna orientation for ground communication and data transmission.

Key Specifications

ParameterValue
ModelC-GDAM/A-11-3A
Output Torque> 3 N·m
Flight Heritage2019
ApplicationMicrosatellite
Dimensions (mm)186 × 133 × 215
Weight (g)1300
Mounting Material2A12
Operating Temperature (°C)−30 to +120
Storage Temperature (°C)−160 to +120

Key Features

  • Ultra-low temperature resistance technology.
  • Lightweight and compact design.
  • High torque-to-volume ratio.
  • Space-grade dust protection technology.

Applications

  • Used for dual-axis antenna pointing and tracking on microsatellite platforms, ensuring stable ground communication and scientific data transmission.
  • See related products in this series

Documentation & Resources

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Frequently Asked Questions

Common questions about Micro Dual-Axis Antenna 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.