Performance of pulsed plasma thruster at low discharge energy
As the size of satellites scales down, low-power and compact propulsion systems such as the pulsed plasma thruster (PPT) are needed for stabilizing these miniature satellites in orbit. Most PPT systems are operated at 2 J or more of discharge energy. In this work, the performance of a PPT with a sid...
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| Main Authors: | , , , , , |
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| Format: | Article |
| Published: |
IOP Publishing
2024
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| Subjects: | |
| Online Access: | http://eprints.um.edu.my/45368/ https://doi.org/10.1088/2058-6272/ad0d52 |
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| Institution: | Universiti Malaya |