Visual Overview
Technical Details
Comprehensive specifications and technical information
Quick Overview
The nano star sensor determines satellite attitude by capturing and identifying stellar images.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | 50 × 50 × 89.4 |
| Weight (g) | 260 |
| Mounting Material | 2A12 T4 |
| Operating Temperature (°C) | −30 to +50 |
| Storage Temperature (°C) | −35 to +60 |
| Communication Interface | RS-422 / CAN |
Key Features
- Precision manufacturing with rapid batch production capability.
- Miniaturized modular design with excellent thermal and structural integration.
- Lightweight, compact, and low power consumption.
- Advanced and stable technical performance indicators.
Applications
- Used for attitude determination and high-dynamic tracking in nanosatellite and microsatellite platforms.
Documentation & Resources
Frequently Asked Questions
Common questions about High-Dynamic Nano Star Sensor
How does the High-Dynamic Nano Star Sensor determine attitude?
It determines satellite attitude by capturing and identifying stellar images, supporting attitude determination and high-dynamic tracking on nanosatellite and microsatellite platforms.
Which interfaces does this star sensor provide?
The sensor communicates over RS-422 and CAN interfaces. It weighs about 260 g and measures 50 x 50 x 89.4 mm.
What temperature range does the sensor support?
It operates from -30 to +50 C and can be stored from -35 to +60 C, with a 2A12 T4 mounting structure.
What makes this star sensor suitable for batch production?
It uses precision manufacturing with rapid batch-production capability and a miniaturized modular design with strong thermal and structural integration.
