Design and Trails on Ionic Plasma Thruster for Aerospace Applications

Abstract:

Ionic plasma thruster is advanced propulsion technology utilized for space applications. Scientific research remains focused on the development of efficient and effective thruster technologies for space exploration. The technology of ionic plasma thruster is notable for its ability to achieve high specific impulse and fuel efficiency. This study outlines our study on plasma and endeavours to enhance Ionic Plasma Thruster through the utilization of innovative methodologies and materials. The experimental setup utilizes electrodes energized by a 1000 kV power module and Lithium-Ion batteries. The design of electrodes is to enhance the concentration of flow electrons for a significant ionization, after ionization the discharged particles (ions) causes the thruster to the system. In addition to ameliorate the thruster, neodymium magnets are strategically positioned, and to expedite the movement of ions and improve the ionization processes. This paper arrays our study and development on plasma ionization and ionic plasma thruster thorough examination of our experimental configuration, methods, and initial findings. Our ongoing research and development efforts aim to expand the technology of ionic plasma thruster, with the goal of enabling more efficient, cost effective and sustainable space exploration missions.

• Periodical: Applied Mechanics and Materials (Volume 935)
• Pages: 53-62
• DOI: https://doi.org/10.4028/p-i1Y4Yv
• Online since: April 2026
• Authors: Yaswanth P. Sai*, Kumar Sah Supen
• Keywords: Discharge Ions, Electrodes, Ionization, Neodymium Magnets, Plasma, Thruster

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