Product Gallery
Visual Overview
Specifications
Technical Details
Comprehensive specifications and technical information
Quick Overview
Flywheels are key actuators in satellite attitude control systems.
Key Specifications
| Parameter | Value |
|---|---|
| Model | C-AOFW-3-1A |
| Rated Momentum | 60 mN·m·s |
| Flight Heritage | Completed in 2017 |
| Application | Microsatellite |
| Dimensions (mm) | 120 × 100 × 95 |
| Weight (kg) | ≤ 1.6 |
| Operating Temperature (°C) | −5 to +45 |
| Storage Temperature (°C) | −10 to +50 |
| Communication Interface | RS-422 |
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 for three-axis attitude control and momentum management in microsatellite platforms.
Documentation & Resources
Support
Frequently Asked Questions
Common questions about Micro Flywheel Combination
What is the rated momentum of the Micro Flywheel Combination?
The model C-AOFW-3-1A provides a rated momentum of 60 mN·m·s for three-axis attitude control and momentum management.
What are the flywheel dimensions and weight?
The unit measures 120 × 100 × 95 mm and weighs no more than 1.6 kg.
What communication interface does it use?
The flywheel combination communicates over RS-422.
What temperature range does it support?
The flywheel combination operates from −5 to +45°C and can be stored from −10 to +50°C.
Does the flywheel combination have flight heritage?
Yes. Its flight qualification was completed in 2017 for microsatellite platforms.
