1 N Single-Component Thruster Assembly - SolarWing.space
Product Details

1 N Single-Component Thruster Assembly

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.

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Comprehensive specifications and technical information

1 N Single-Component Thruster Assembly

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

ParameterValue
Dimensions (mm)Φ58 × 128
Mass (g)300 ± 20
PropellantHydrazine
Specific Impulse200 s
Design Life15 years
Valve Drive Voltage28 ± 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.
  • See related products in this series

Documentation & Resources

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Frequently Asked Questions

Common questions about 1 N Single-Component Thruster Assembly

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.