Visual Overview
Technical Details
Comprehensive specifications and technical information
Quick Overview
The 1 N Single-Component Thruster is a critical actuator for satellite attitude and orbit control, designed for commercial aerospace applications. It offers high reliability, long service life, and cost efficiency, supporting batch production for constellation missions and on-orbit propulsion platforms.
Key Specifications
| Parameter | Value |
|---|---|
| Dimensions (mm) | Φ58 × 128 |
| Mass (g) | 300 ± 20 |
| Propellant | Hydrazine |
| Specific Impulse | 200 s |
| Design Life | 15 years |
| Valve Drive Voltage | 28 ± 3 V DC |
Key Features
- High reliability and low cost.
- Excellent adaptability to space environments.
- Compatible with on-orbit application platforms.
Applications
- Used for small satellite attitude and orbit control in on-orbit propulsion platforms, with proven flight heritage and high-volume production capability.
Documentation & Resources
Frequently Asked Questions
Common questions about 1 N Single-Component Thruster Assembly
What thrust and propellant does the 1 N thruster use?
It is a 1 N single-component thruster fueled by hydrazine, with a specific impulse of 200 s for satellite attitude and orbit control.
What is the design life of this thruster?
The thruster is qualified for a design life of 15 years, supporting long-duration missions and on-orbit propulsion platforms.
What drive voltage does the valve need?
The valve operates on a drive voltage of 28 ± 3 V DC.
What are the thruster dimensions and mass?
The unit has a Φ58 × 128 mm envelope and a mass of 300 ± 20 g.
Is the 1 N thruster suitable for constellations?
Yes. It is designed for commercial aerospace use and supports batch production for constellation missions and on-orbit propulsion platforms.
