Lab-on-PCB solid propellant microthruster with multi-mode thrust capabilities

In the realm of nano/microsatellite clustering, the demand for microthrusters is steadily growing. Solid propellant microthrusters, recognized for their lightweight build and structural simplicity, carry significant commercial promise. However, existing solid propellant microthrusters manufactured u...

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Bibliographic Details
Published in:Lab on a chip 2024-09, Vol.24 (19), p.4558-457
Main Authors: Lee, Jeongrak, Kim, Seonghyeon, Jo, Hanseong, Lee, Anna
Format: Article
Language:English
Subjects:
Chambers
Circuit boards
Clustering
Electronic control
Mass production
Microsatellites
Printed circuits
Solid propellants
Structural stability
Surface stability
Thrust
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Summary:In the realm of nano/microsatellite clustering, the demand for microthrusters is steadily growing. Solid propellant microthrusters, recognized for their lightweight build and structural simplicity, carry significant commercial promise. However, existing solid propellant microthrusters manufactured using MEMS technology encounter notable issues such as inconsistent thrust generation positions, limited thrust profiles, and issues related to productivity, scalability, and durability. In this study, we propose a novel shared-chamber solid-propellant microthruster design that consistently produces thrust at a designated position and accommodates multiple thrust modes. The components and fabrication of this thruster were developed using lab-on-printed-circuit-board (PCB) technology and PCB surface mount technology, showcasing enhanced structural stability, scalability, and potential for mass production. Our ignition and combustion experiments confirmed the repeatability of the unit operation, a fundamental feature of this innovative microthruster. Furthermore, we successfully implemented and evaluated the power mode for increased thrust and the continuous mode for prolonged operational duration. Integrating the lab-on-PCB-based shared-chamber solid propellant microthruster with propulsion and electronic control systems holds promising potential for future satellite missions. This study presents a novel concept of a shared-chamber solid-propellant microthruster generating multi-mode thrust in a fixed position. Utilizing the lab-on-PCB technique, it shows improved scalability, mass production potential, and performance.
ISSN:1473-0197
1473-0189
1473-0189
DOI:10.1039/d4lc00516c