Visual Overview
Technical Details
Comprehensive specifications and technical information
High-Dynamic Nano Star Sensor
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.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about High-Dynamic Nano Star Sensor
How does the High-Dynamic Nano Star Sensor interface with a satellite's onboard computer and other electronics?
Our High-Dynamic Nano Star Sensor typically interfaces with the onboard computer via a standard serial interface like RS-422 or a SpaceWire link. Data is transmitted in a defined packet format, including star identification, position, and attitude information. Power is supplied through a dedicated power bus. The sensor may also have discrete I/O for synchronization or triggering events with other satellite electronics.
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.