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Thrust Analysis of DIY Ion Thruster by asaboor098 is a document available to read on EtoBox.

This document presents a study on the thrust generated by a DIY ion thruster, focusing on electronic propulsion technology used for satellite movement. The author details the mathematical modeling of thrust, experimental setup, and observations, concluding that thrust is influenced by the mass of the propellant and the distance between electrodes. The findings suggest that the experiment can be replicated for improved accuracy and precision in ion propulsion research.

Author
asaboor098
Language
EN