Research and Development Trends of Pulsed Plasma Thruster for Small Satellites

A pulsed plasma thruster (PPT) is an electric thruster that generates thrust using electromagnetic fields.Due to its relatively low power requirements and simple design, the PPT has been widely utilized for attitude control and orbit transfers in small satellites.In recent years, the increasing diversification of space missions such as small satellite constellations and space-based internet has driven the demand for low-cost CubeSats.Consequently, pulsed plasma thrusters (PPTs) are being actively employed as propulsion systems for the small satellites.In this paper, the research and development status of PPTs from early prototypes to recent thrusters designed for small satellites, is reviewed, categorized by development year and power consumption.Furthermore, the utilization of PPTs is summarized based on satellite missions.

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Publication Details

Journal
Journal of the Korean Society of Propulsion Engineers
Published
2025-06-30
DOI
https://doi.org/10.6108/kspe.2025.29.4.011
Citations
1
Primary Topic
Plasma Diagnostics and Applications
Type
article
Field-Weighted Citation Impact
0.73
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article

Research and Development Trends of Pulsed Plasma Thruster for Small Satellites

Holak Kim, S. G. Baek
1 citations
Journal of the Korean Society of Propulsion Engineers
Plasma Diagnostics and Applications
0.73
article

Research and Development Trends of Pulsed Plasma Thruster for Small Satellites

Holak Kim, S. G. Baek
article en
1 citations

Abstract

A pulsed plasma thruster (PPT) is an electric thruster that generates thrust using electromagnetic fields.Due to its relatively low power requirements and simple design, the PPT has been widely utilized for attitude control and orbit transfers in small satellites.In recent years, the increasing diversification of space missions such as small satellite constellations and space-based internet has driven the demand for low-cost CubeSats.Consequently, pulsed plasma thrusters (PPTs) are being actively employed as propulsion systems for the small satellites.In this paper, the research and development status of PPTs from early prototypes to recent thrusters designed for small satellites, is reviewed, categorized by development year and power consumption.Furthermore, the utilization of PPTs is summarized based on satellite missions.

Journal of the Korean Society of Propulsion EngineersVol. 29(3)
Pusan National University (KR)
Openalex Percentile: Top 24%
Plasma Diagnostics and Applications
0.73
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Research and Development Trends of Pulsed Plasma Thruster for Small Satellites — Holak Kim, S. G. Baek · Journal of the Korean Society of Propulsion Engineers (2025) | TGRS Research Map | TGRS