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Comprehensive specifications and technical information
Quick Overview
The solar array drive mechanism (SADM) enables satellite solar panels to rotate for sunlight acquisition, tracking, and power optimization.
Key Specifications
| Parameter | Value |
|---|---|
| Model | C-SADM-4-2A |
| Transmission Power | ≥ 1 kW |
| Flight Heritage | Prototype stage |
| Application | Microsatellite |
| Dimensions (mm) | Ø100 × 160 |
| Weight (g) | 1200 |
| Mounting Material | TC4 |
| Operating Temperature (°C) | −25 to +65 |
| Storage Temperature (°C) | −30 to +70 |
Key Features
- Integrated electromechanical structural design.
- Lightweight and compact form factor.
- High power-to-volume ratio.
Applications
- Used for solar array deployment and power transfer in microsatellite platforms requiring efficient and reliable sun-tracking mechanisms.
Documentation & Resources
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Frequently Asked Questions
Common questions about Micro Integrated Electromechanical Solar Array Drive Mechanism
How much power can this solar array drive mechanism transfer?
The model C-SADM-4-2A transmits at least 1 kW of power while rotating the solar array for sun tracking.
What are the mechanism dimensions and weight?
The unit measures Ø100 × 160 mm and weighs about 1200 g on a TC4 titanium-alloy mounting.
What temperature range does it support?
It operates from −25 to +65°C and can be stored from −30 to +70°C.
What is the current development status?
The mechanism is currently at the prototype stage rather than in flight service.
What is the mechanism used for?
It rotates satellite solar panels for sunlight acquisition, tracking, and power transfer on microsatellite platforms.
