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Technical Details
Comprehensive specifications and technical information
C-GLV-3 Self-Locking Valve
Quick Overview
The C-GLV-3 Self-Locking Valve is a cost-effective and compact product developed based on the GLV-3 low-friction self-locking design for commercial satellite propulsion systems. It is typically installed between the propellant tank and the thruster or as an upstream control valve. The valve is used to open, close, or isolate specific propulsion branches, ensuring the safety and reliability of the propulsion system.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | Φ31 × 174 × 53 |
| Mass (g) | 350 ± 10 |
| Design Life | 8 years |
| Valve Drive Voltage | 24 V DC – 31 V DC |
Key Features
- Low friction torque and axial flow design.
- High mechanical reliability with self-locking capability.
- Low cost, lightweight, and low power consumption.
- Excellent adaptability to space environments.
Applications
- Used in commercial satellite propulsion systems for propellant flow control.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about C-GLV-3 Self-Locking Valve
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.