The Injector Plate Design of a 500lbf Kerosene Base / H2O2 Liquid Rocket Engine
碩士 === 國立成功大學 === 航空太空工程學系 === 104 === For kerosene base fuel and H2O2 propellant system in liquid rocket engine design, two-stage impinging injection provides adequate mixing between propellants and excellent characteristic velocity after burning. In this thesis study, a two-stage impinging injecto...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2016
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| Online Access: | http://ndltd.ncl.edu.tw/handle/8mqrp4 |