Visual Overview
Technical Details
Comprehensive specifications and technical information
Quick Overview
The Small Satellite Positional Orbit Control Propulsion Module adopts a monopropellant propulsion system utilizing green, non-toxic propellants such as HAN or ADN. It features a blowdown mode with a single-tank configuration, ensuring compact structure, safety, and ease of integration for small satellite orbit and attitude control missions.
Key Specifications
| Parameter | Value |
|---|---|
| Dry Mass (kg) | 5.7 |
| Propellant | HAN / ADN |
| Operating Temperature (°C) | 0–50 |
| Storage Temperature (°C) | −5–55 |
Key Features
- Monopropellant propulsion system.
- Uses non-toxic HAN or ADN propellant.
- Blowdown mode with single-tank structural design.
Applications
- Successfully applied in the KX-1N satellite, demonstrating proven in-orbit flight performance.
Documentation & Resources
Frequently Asked Questions
Common questions about Small Satellite Positional Orbit Control Propulsion Module
What propellant does this orbit control module use?
It uses a green, non-toxic monopropellant such as HAN or ADN in a monopropellant propulsion system for small satellites.
What is the module dry mass?
The module has a dry mass of about 5.7 kg.
How is the propulsion system configured?
It uses a blowdown mode with a single-tank structural design for a compact, safe, easily integrated package.
What temperature range does the module support?
The HAN/ADN module operates from 0 to 50°C and can be stored from −5 to +55°C.
Does the module have flight heritage?
Yes. It was successfully applied on the KX-1N satellite, demonstrating proven in-orbit flight performance.
