Visual Overview
Technical Details
Comprehensive specifications and technical information
2 MPa Micro Pressure Sensor
Quick Overview
The 2 MPa Micro Pressure Sensor is an essential unit for measuring propellant tank pressure in satellite propulsion systems. It employs a metallic elastic diaphragm sensing principle, achieving high performance at a low cost. The sensor is lightweight, compact, precise, and energy-efficient, making it ideal for micro- and small-satellite propulsion applications.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | 26 × 26 × 62 |
| Mass (g) | 60 |
| Mounting Material | 316L |
| Operating Temperature (°C) | −20 to +50 |
| Storage Temperature (°C) | −40 to +125 |
| Communication Interface | Y4–4ZJLM |
Key Features
- Manufactured with advanced ion-beam etching and micro-machining technology.
- Integrated electromechanical design with high integration level.
- Lightweight, compact, high accuracy, and low power consumption.
- Excellent adaptability to harsh space environments.
Applications
- Used for propellant tank pressure monitoring in satellite propulsion systems.
Related Products
- See related products in this series
Documentation & Resources
Frequently Asked Questions
Common questions about 2 MPa Micro Pressure Sensor
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.