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Comprehensive specifications and technical information
Quick Overview
The magnetic torquer is an essential actuator in satellite attitude control systems.
Key Specifications
| Parameter | Value |
|---|---|
| Model | C-GMAT-0.5 / C-GMAT-1 / C-GMAT-10 / CGMAT(I)-10 |
| Magnetic Moment | 0.5 A·m² / 1 A·m² / 10 A·m² |
| Flight Heritage | 2015–2019 (multiple flight missions) |
| Application | Pico- and microsatellites |
Key Features
- Low-cost design and implementation.
- Small residual magnetic moment and high linearity.
- Lightweight, compact, and low power consumption.
- Excellent adaptability to space environmental conditions.
Applications
- Used for magnetic attitude control and momentum unloading in pico- and microsatellite attitude control subsystems.
Documentation & Resources
Support
Frequently Asked Questions
Common questions about Micro Magnetic Torquer
What magnetic moment options does this torquer offer?
The series offers magnetic moments of 0.5, 1, and 10 A·m² across the C-GMAT-0.5, C-GMAT-1, C-GMAT-10, and CGMAT(I)-10 models.
What is the magnetic torquer used for?
It provides magnetic attitude control and momentum unloading in pico- and microsatellite attitude control subsystems.
What makes the torquer suitable for small satellites?
It offers a small residual magnetic moment, high linearity, and low power consumption in a lightweight, compact package.
Does the magnetic torquer have flight heritage?
Yes. It has flight heritage across multiple missions from 2015 to 2019 on pico- and microsatellites.
