Design and Analysis of a Micro–Electro-Mechanical System Thruster for Small Satellites and Low-Thrust Propulsion

Design and Analysis of a Micro–Electro-Mechanical System Thruster for Small Satellites and Low-Thrust Propulsion

As a cost-effective and versatile solution, small satellites are increasingly being considered for space exploration. However, one of the major challenges in deploying small satellites for high total impulse missions, particularly deep space exploration, lies in the propulsion system. These missions...

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Bibliographic Details
Main Authors: Yubin Zhong, Fabrizio Ponti, Francesco Barato, Guojun Xia, Siyu Li, Xiao Zhang, Tao Wu
Format: Article
Language:English
Published: MDPI AG 2025-02-01
Series:Aerospace
Subjects:
MEMS propulsion
small satellites
green propellant
low-thrust propulsion
spacecraft design
Online Access:https://www.mdpi.com/2226-4310/12/3/172
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