Development of a Highly Reliable Data Acquisition System for Hybrid Rocket Ground Static-Burn Test Facility
碩士 === 國立交通大學 === 工學院精密與自動化工程學程 === 104 === Reaction in combustion chamber of rocket propulsion generates thrust and, simultaneously, induces high temperature and pressure which can cause burnthrough of structure or even destruction. In addition to rigorous design, analysis and simulation, comprehen...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2015
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| Online Access: | http://ndltd.ncl.edu.tw/handle/04245631605892496872 |