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Review | Open Access

Thrust-vectoring schemes for electric propulsion systems: A review

Andrei SHUMEIKOa,b( ), Victor TELEKHb, Sergei RYZHKOVc
R&D Department, Advanced Propulsion Systems LLC, Moscow 121205, Russia
Department of Plasma Power Plants, Bauman Moscow State Technical University, Moscow 105005, Russia
Department of Thermal Physics, Bauman Moscow State Technical University, Moscow 105005, Russia

Peer review under responsibility of Editorial Committee of CJA

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Abstract

Thrust-vectoring capability has become a critical feature for propulsion systems as space missions move from static to dynamic. Thrust-vectoring is a well-developed area of rocket engine science. For electric propulsion, however, it is an evolving field that has taken a new leap forward in recent years. A review and analysis of thrust-vectoring schemes for electric propulsion systems have been conducted. The scope of this review includes thrust-vectoring schemes that can be implemented for electrostatic, electromagnetic, and beam-driven thrusters. A classification of electric propulsion schemes that provide thrust-vectoring capability is developed. More attention is given to schemes implemented in laboratory prototypes and flight models. The final part is devoted to a discussion on the suitability of different electric propulsion systems with thrust-vectoring capability for modern space mission operations. The thrust-vectoring capability of electric propulsion is necessary for inner and outer space satellites, which are at a disadvantage with conventional unidirectional propulsion systems due to their limited maneuverability.

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Chinese Journal of Aeronautics

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Cite this article:
SHUMEIKO A, TELEKH V, RYZHKOV S. Thrust-vectoring schemes for electric propulsion systems: A review. Chinese Journal of Aeronautics, 2025, 38(6). https://doi.org/10.1016/j.cja.2025.103401

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Received: 12 May 2024
Revised: 16 June 2024
Accepted: 08 July 2024
Published: 13 January 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).