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Comprehensive specifications and technical information
Quick Overview
The monolithic solar sensor uses an APS image sensor as the photoelectric conversion detector.
Key Specifications
| Parameter | Value |
|---|---|
| Model | C-SS-SiC-ANA/B-2B |
| Measurement Accuracy | 0.05° (3σ) |
| Flight Heritage | Completed qualification |
| Application | Low Earth Orbit satellites |
| Dimensions (mm) | 35 × 35 × 15 |
| Weight (g) | 50 |
| Mounting Material | 2A12 T4 |
| Operating Temperature (°C) | −30 to +45 |
| Storage Temperature (°C) | −35 to +55 |
| Data Update Rate | ≥15 Hz |
| Communication Interface | RS-422 / CAN |
| Design Life | 2 years |
Key Features
- Low-cost design and implementation.
- Integrated opto-electronic structure with high integration.
- Lightweight and compact design.
- High adaptability to space environmental conditions.
Applications
- Used for solar vector detection and attitude determination in low-orbit satellite systems.
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Frequently Asked Questions
Common questions about Monolithic Solar Sensor
What detector does the Monolithic Solar Sensor use?
It uses an APS image sensor as the photoelectric conversion detector and achieves a measurement accuracy of 0.05 degrees (3-sigma) with a data update rate of at least 15 Hz.
Which interfaces does the solar sensor provide?
It supports RS-422 and CAN interfaces. The sensor is compact at 35 x 35 x 15 mm and lightweight at about 50 g.
What is the design life and target orbit?
Model C-SS-SiC-ANA/B-2B has a 2-year design life, has completed qualification, and is used in low Earth orbit satellite systems.
What temperature range does it support?
It operates from -30 to +45 C and can be stored from -35 to +55 C, with a 2A12 T4 mounting material.
