Visual Overview
Technical Details
Comprehensive specifications and technical information
Quick Overview
The Tiny Satellite Position-Controlled Propulsion Module is a compact monopropellant propulsion system using non-toxic ADN-based propellant. Designed for micro and small satellite constellations, it enables efficient orbit and attitude control with rapid integration, batch production capability, and cost-effective deployment.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | 600 × 400 × 400 |
| Dry Mass (kg) | 3.6 |
| Propellant | ADN |
| Operating Temperature (°C) | 0–50 |
| Storage Temperature (°C) | −5–55 |
Key Features
- Monopropellant propulsion system.
- Utilizes a green, non-toxic ADN propellant.
- Supports pre-integration and modular delivery configuration.
Applications
- Successfully applied in the NX-1 satellite, meeting the requirements of small satellite constellation deployment, rapid integration, and low-cost assembly with proven flight experience.
Documentation & Resources
Frequently Asked Questions
Common questions about Tiny Satellite Position-Controlled Propulsion Module
What propellant does this position control module use?
It uses a compact monopropellant propulsion system running on non-toxic, green ADN propellant.
What are the module dry mass and dimensions?
The module has a dry mass of about 3.6 kg and measures 600 × 400 × 400 mm.
What temperature range does it operate across?
The ADN-based module operates from 0 to 50°C and can be stored from −5 to +55°C.
Is the module suited to satellite constellations?
Yes. It supports rapid integration, batch production, and low-cost assembly for micro and small satellite constellations.
Does the module have flight heritage?
Yes. It was successfully applied on the NX-1 satellite with proven flight experience.
