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Recent efforts have been made to develop hydrogen‐oxygen propellant (HOP)‐based microthruster systems. When compared to other propulsion systems, the HOP‐based system has several advantages, including low cost, nontoxicity, ease of use and recyclability. The present work focuses on developing microthrusters based on hydrogen‐oxygen chemical combustion. The proposed HOP‐based microthruster is based...
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