Design and Implementation of Strand Burner Chamber for Burning Characterization of Solid Propellant with Preliminary Experimental Results
碩士 === 國立交通大學 === 機械工程系所 === 104 === Regression rate in solid rocket motor is the most important factor for the sounding rocket. The pressure stability which determined by the solid rocket fuel regression rate as the function of chamber pressure. Sugar fuel, Sorbitol based (KNSB), with chemical comp...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2016
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| Online Access: | http://ndltd.ncl.edu.tw/handle/41438083155142465122 |