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Comprehensive specifications and technical information
Quick Overview
The reaction wheel is a key actuator in satellite attitude control systems.
Key Specifications
| Parameter | Value |
|---|---|
| Model | C-GRWMI-130-0.5A |
| Rated Momentum | 0.5 N·m·s |
| Flight Heritage | First flight in 2012 |
| Application | Micro/Nanosatellite |
| Dimensions (mm) | 135 × 135 × 110 |
| Weight (kg) | 2.1 ± 0.3 |
| Operating Temperature (°C) | −5 to +45 |
| Storage Temperature (°C) | −10 to +50 |
| Communication Interface | Analog Interface |
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 precision attitude control and momentum management in micro and nanosatellite attitude control systems.
Documentation & Resources
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Frequently Asked Questions
Common questions about 130 Standard Reaction Wheel
What is the rated momentum of the 130 Standard Reaction Wheel?
The model C-GRWMI-130-0.5A provides a rated momentum of 0.5 N·m·s for precision attitude control and momentum management.
What are the wheel dimensions and weight?
The reaction wheel measures 135 × 135 × 110 mm and weighs 2.1 ± 0.3 kg.
What communication interface does it use?
The wheel uses an analog interface.
What temperature range does it support?
The 130 wheel operates from −5 to +45°C and can be stored from −10 to +50°C.
Does the 130 reaction wheel have flight heritage?
Yes. It achieved its first flight in 2012 on micro- and nanosatellite missions.
