Spray Characteristics of Nitrous Oxide Pressure-Swirl Injector for Hybrid Rockets
碩士 === 國立成功大學 === 航空太空工程學系 === 103 === Self-pressurizing rocket propellants are currently gaining popularity in the propulsion community, especially in hybrid rocket applications. Self-pressurizing oxidizers with its high vapor pressure, can be driven out from the storage tank and injected into comb...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
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2015
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| Online Access: | http://ndltd.ncl.edu.tw/handle/96277526444621331739 |