Development of a Global Model for the Analysis of Plasma in an Atmosphere-Breathing Cathode-Less Thruster

This study investigates the preliminary propulsive performances of a cathode-less plasma thruster with air as its propellant. The analysis is carried out through a global model and simulates a thruster over a power range of 0 to 50 W. The developed code considers a set of 177 chemical reactions invo...

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Bibliographic Details
Main Authors: Simone Dalle Fabbriche, Nabil Souhair, Mirko Magarotto, Raoul Andriulli, Enrico Corti, Fabrizio Ponti
Format: Article
Language:English
Published: MDPI AG 2023-04-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/5/389