Visual Overview
Technical Details
Comprehensive specifications and technical information
Micro-Nano Flywheel and Magnetic Torquer Assembly
Quick Overview
Both flywheels and magnetic torquers are key actuators in satellite attitude control systems.
Key Specifications
| Parameter | Value |
|---|---|
| Model | C-AOWM-3-3-1A |
| Rated Torque | 0.4 mN·m·s |
| Flight Heritage | Completed in 2015 |
| Application | Nanosatellite |
| Dimensions (mm) | 90 × 90 × 40 |
| Weight (g) | ≤ 380 |
| Operating Temperature (°C) | −5 to +45 |
| Storage Temperature (°C) | −10 to +50 |
| Communication Interface | CAN |
Key Features
- Low-cost design and implementation technology.
- Integrated electromechanical design with high compactness.
- Lightweight, small size, and low power consumption.
- Excellent adaptability to space environments.
Applications
- Used in nanosatellite attitude control systems integrating torque and momentum management functions.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about Micro-Nano Flywheel and Magnetic Torquer Assembly
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.