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Technical Details
Comprehensive specifications and technical information
Solid Cold-Gas Micropropulsion Module
Quick Overview
The Solid Cold-Gas Micropropulsion Module is a new-generation propulsion system based on solid gas-generating propellant technology. It consists of a gas generator, storage chamber, control circuitry, and sensors. The solid gas generator produces the required cold gas, which is supplied to the thruster assembly to generate precise thrust and torque for micro- and nano-satellite attitude and orbit control.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | 96 × 96 × 98 |
| Mass (g) | 1200 |
| Total Impulse | 80 N·s |
| Mounting Material | TC4 (Titanium Alloy) |
| Operating Temperature (°C) | −15 to +55 |
| Storage Temperature (°C) | −40 to +95 |
| Communication Interface | RS-422 / CAN |
Key Features
- No high-pressure components.
- Long storage life.
- Lightweight, compact, and low power consumption.
- Modular design with strong scalability.
Applications
- Used in micro- and nano-satellite attitude and orbit control systems for long-term storage and reliable cold-gas propulsion.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about Solid Cold-Gas Micropropulsion 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.