Visual Overview
Technical Details
Comprehensive specifications and technical information
Quick Overview
The Micro-Nano Satellite Position Control Integrated Module adopts a compact monopropellant propulsion system using green propellant. It provides reliable and efficient attitude and orbit control capabilities for micro and nano satellites through a simplified structural design and high system reliability.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | 280 × 250 × 400 |
| Dry Mass (kg) | 1.8 |
| Propellant | HAN-Based Green Propellant |
| Operating Temperature (°C) | 5–60 |
| Storage Temperature (°C) | 0–65 |
Key Features
- Monopropellant propulsion system.
- Uses a non-toxic propellant (HAN-based).
- Simple structure with high reliability.
Applications
- Successfully applied in PN-1A and PN-2A satellites with verified flight experience.
Documentation & Resources
Frequently Asked Questions
Common questions about Micro-Nano Satellite Position Control Integrated Module
What propellant does this position control module use?
It uses a HAN-based green, non-toxic monopropellant in a compact monopropellant propulsion system for micro and nano satellites.
What are the module dry mass and dimensions?
The module has a dry mass of about 1.8 kg and measures 280 × 250 × 400 mm.
What temperature range does it operate across?
It operates from 5 to 60°C and can be stored from 0 to 65°C.
Does the module have flight heritage?
Yes. It has been successfully applied on the PN-1A and PN-2A satellites with verified flight experience.
What control functions does the module provide?
It delivers reliable attitude and orbit control, including station-keeping and orbit adjustments, through a simplified, high-reliability structure.
