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Technical Details
Comprehensive specifications and technical information
ADN-Based Single-Component Micro-Propulsion Module
Quick Overview
The ADN-Based Single-Component Micro-Propulsion Module utilizes a high-energy, non-toxic ADN propellant. Through a solid gas generator, it supports pre-packaged and plug-and-play deployment, allowing quick installation and reliable operation. The system provides high total impulse and thrust output, making it suitable for micro- and nano-satellite rapid orbit adjustment, long-term attitude control, and orbit maintenance missions.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | 110 × 100 × 94 |
| Mass (g) | 1300 |
| Total Impulse | 800 N·s |
| Service Life (years) | ≥ 4 |
| Operating Temperature (°C) | 0–50 |
| Storage Temperature (°C) | −5–55 |
| Communication Interface | RS-422 / CAN |
Key Features
- Pre-packaged configuration.
- Plug-and-play capability.
- High total impulse and strong thrust performance.
- Modular design with excellent scalability.
Applications
- Used in micro- and nano-satellite propulsion systems, particularly for rapid orbit transfer, attitude maintenance, and orbital maneuvering, with verified flight performance since 2020.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about ADN-Based Single-Component Micro-Propulsion Module
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.
What documentation and support is available?
Complete technical documentation includes user manuals, interface control documents, test reports, and application notes. Our engineering team provides integration support, training, and ongoing technical assistance throughout the mission lifecycle.