A Study on 2.75 Inch High burning Rate Rocket Igniter
碩士 === 國防大學理工學院 === 兵器系統工程碩士班 === 101 === A front-end rocket ignition system is investigated. This system can be operated at low voltage 9V for 2.75 inch rocket propellant instant detonation. When the igniter is detonated, the output temperature, pressure, burning rate and heat flux are critical to...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2013
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| Online Access: | http://ndltd.ncl.edu.tw/handle/75642504127615076401 |