Experimental and Numerical Investigation of N2O Flow Feeding System in a Hybrid Rocket

碩士 === 國立交通大學 === 機械工程學系 === 100 === Hybrid rocket propulsion has attracted much attention recently mainly because of its capability of thrust profiling, in addition to its safe and green operation. To realize thrust control, the easiest way is to accurately control the flow rate of oxidizer flowing...

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Bibliographic Details
Main Authors: Chuang, Kang-Ming, 莊康旻
Other Authors: Wu, Jong-Shinn
Format: Others
Language:en_US
Published: 2012
Online Access:http://ndltd.ncl.edu.tw/handle/56628900210202698679