Design and Performance Analysis of A MEMS-based Hydrazine Microthruster
博士 === 國立成功大學 === 航空太空工程學系碩博士班 === 98 === MEMS techniques were adopted to miniaturize the conventional hydrazine monothruster in this thesis research. Based on the reaction control requirements of the micro- and nano-satellites, the targeted hydrazine microthruster was designed to provide millinewto...
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| Format: | Others |
| Language: | en_US |
| Published: |
2010
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| Online Access: | http://ndltd.ncl.edu.tw/handle/13968732935534501887 |