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Technical Details
Comprehensive specifications and technical information
Tiny Ultra-High-Pressure Cold-Gas Propulsion System
Quick Overview
The Tiny Ultra-High-Pressure Cold-Gas Propulsion System reduces a 60 MPa high-pressure gas source to a lower working pressure through a multi-stage regulator, enabling micro cold-gas thrusters to generate milli-Newton (mN) thrust levels. Designed for spacecraft requiring high precision and compact propulsion, this system offers advantages in total impulse, structural integration, power efficiency, and reliability. The technology incorporates ultra-high-pressure storage, lightweight pressure-reduction structures, and advanced sealing to ensure excellent adaptability and long-term stability in space environments.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | 190 × 430 × 190 |
| System Mass (kg) | ≤ 2 |
| Total Impulse | > 700 N·s |
| Power Consumption | < 1 W |
| Mounting Material | 1Cr18Ni9Ti |
| Operating Temperature (°C) | −5 to +65 |
| Storage Temperature (°C) | −5 to +70 |
| Electrical Interface | Dual FY1–2 connectors |
| Thrust Range | 10–200 mN |
Key Features
- High total impulse and reliability.
- Ultra-high-pressure storage and precise multi-stage pressure regulation.
- Lightweight, compact, and energy-efficient design.
- Excellent environmental adaptability for space missions.
Applications
- Used for micro-satellite attitude control, orbit maintenance, and formation-flying missions requiring milli-Newton thrust precision.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about Tiny Ultra-High-Pressure Cold-Gas Propulsion System
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.