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Technical Details
Comprehensive specifications and technical information
0.2 N Single-Component Thruster Assembly
Quick Overview
The 0.2 N Single-Component Thruster is a key actuator for satellite attitude and orbit control. Designed with a compact structure and high efficiency, it ensures precise thrust performance and high reliability. The thruster employs a low-friction valve design to extend operational life and features advanced micro-scale fabrication and long-life sealing technology, making it ideal for micro- and small-satellite propulsion applications.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | Φ48 × 92 |
| Mass (g) | 175 ± 10 |
| Propellant | Hydrazine |
| Specific Impulse | 190 s |
| Design Life | 5 years |
| Valve Drive Voltage | 28 ± 3 V DC |
Key Features
- Precision thrust control.
- Electromagnetic valve with frictionless operation and high reliability.
- Lightweight, compact, and low power consumption.
- Excellent adaptability to space environments.
Applications
- Used for micro-satellite attitude and orbit control.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about 0.2 N Single-Component Thruster Assembly
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.