Оптимизация, испытания и диагностика миниатюрных Холл подруливающие устройства

Overview

This article presents a protocol for testing and optimizing space propulsion systems, specifically focusing on miniaturized Hall-type thrusters. The methodology involves automated systems for diagnostics and performance evaluation in a controlled environment.

Key Study Components

Area of Science

• Space propulsion systems
• Electric propulsion thrusters
• Automated diagnostic systems

Background

• The research is conducted at the Space Propulsion Center in Singapore.
• It focuses on the testing of specialized electric propulsion thrusters.
• Facilities include space environment simulation for various testing purposes.
• Lifetime testing of thrusters is a primary focus.

Purpose of Study

• To evaluate the performance of miniaturized Hall-type thrusters.
• To assess the effects of plasma damage on thruster components.
• To develop automated systems for remote diagnostics.

Methods Used

• Automated systems for testing propulsion modules.
• Hardware-software integration for smart diagnostics.
• Space environment simulation facilities for testing.
• Extended firing of thrusters to evaluate performance.

Main Results

• Development of a robust methodology for thruster testing.
• Identification of plasma damage effects on thruster components.
• Successful integration of automated systems for diagnostics.
• Establishment of a reliable testing environment.

Conclusions

• The protocol enhances the testing and optimization of space propulsion systems.
• Automated diagnostics improve efficiency and accuracy.
• Findings contribute to advancements in electric propulsion technology.

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