Numerical and Experimental Investigation of Single-Port Hybrid Rocket Propulsion System with Nitrous Oxide and Hydroxyl-terminated Polybutadiene (HTPB) using Mixing Enhancer(s)
博士 === 國立交通大學 === 機械工程系所 === 103 === Recently, hybrid rocket propulsion has attracted much attention because of many advantages, including high safety, high performance and low cost. Hybrid rocket system has better propulsion performance as compared to solid rocket system, but combustion efficiency...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2015
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| Online Access: | http://ndltd.ncl.edu.tw/handle/28dagq |