Small Satellite Positional Orbit Control Propulsion Module - SolarWing.space
Product Details

Small Satellite Positional Orbit Control Propulsion Module

The Small Satellite Positional Orbit Control Propulsion Module adopts a monopropellant propulsion system utilizing green, non-toxic propellants such as HAN or ADN. It features a blowdown mode with a single-tank configuration, ensuring compact structure, safety, and ease of integration for small satellite orbit and attitude control missions.

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Comprehensive specifications and technical information

Small Satellite Positional Orbit Control Propulsion Module

Quick Overview

The Small Satellite Positional Orbit Control Propulsion Module adopts a monopropellant propulsion system utilizing green, non-toxic propellants such as HAN or ADN. It features a blowdown mode with a single-tank configuration, ensuring compact structure, safety, and ease of integration for small satellite orbit and attitude control missions.

Key Specifications

ParameterValue
Dry Mass (kg)5.7
PropellantHAN / ADN
Operating Temperature (°C)0–50
Storage Temperature (°C)−5–55

Key Features

  • Monopropellant propulsion system.
  • Uses non-toxic HAN or ADN propellant.
  • Blowdown mode with single-tank structural design.

Applications

  • Successfully applied in the KX-1N satellite, demonstrating proven in-orbit flight performance.
  • See related products in this series

Documentation & Resources

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Frequently Asked Questions

Common questions about Small Satellite Positional Orbit Control Propulsion Module

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.