Visual Overview
Technical Details
Comprehensive specifications and technical information
Low-Power Hall Thruster
Quick Overview
The Low-Power Hall Thruster is designed for micro- and nanosatellite orbit transfer and station-keeping missions. It uses inert gas as the propellant and features a lightweight, compact design with high reliability and long operational life. The 300 W and 600 W variants are optimized for low-Earth orbit (LEO) constellations, including broadband communication and remote-sensing satellite missions.
Key Specifications
ET-H300-1 Model
| Parameter | Value |
|---|---|
| Power | 300 W |
| Dimensions | 144 × 114 × 91 mm |
| Mass | 1.2 kg |
| Propellant | High-purity Xenon |
| Operating Temperature | −40 to +80 °C |
| Mechanical Interface | 6 × φ 4.5 |
ET-H600-1 Model
| Parameter | Value |
|---|---|
| Power | 600 W |
| Dimensions | 190 × 160 × 110 mm |
| Mass | 2.0 kg |
| Propellant | High-purity Xenon |
| Operating Temperature | −40 to +80 °C |
| Mechanical Interface | 6 × φ 4.5 |
Key Features
- Lightweight and compact structure
- High reliability and stable operation
- Long service life
- Suitable for orbit transfer and station-keeping missions
- Available in 300W and 600W variants
- Optimized for LEO constellations
Technical Details
Architecture & Design
The Low-Power Hall Thruster uses inert gas (high-purity Xenon) as propellant and employs Hall effect acceleration principles for efficient thrust generation. The design is optimized for micro- and nanosatellite applications with emphasis on:
- Compact form factor suitable for small satellite platforms
- High specific impulse for efficient propellant utilization
- Long operational lifetime for extended missions
- Stable performance across wide temperature ranges
Flight Heritage
- ET-H300-1 and ET-H600-1 achieved first flight in 2019
- Demonstrated stable and efficient in-orbit performance
- Validated for LEO constellation missions
Applications
- Micro- and nanosatellite orbit transfer
- Station-keeping missions
- Constellation adjustment in low Earth orbit
- Broadband communication satellites
- Remote-sensing satellite missions
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about Low-Power Hall Thruster
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.