摘要
NEPE high energetic solid propellant has been in prospect of application for its excellant comprehensive properties. The burning rate and pressure exponent were adjusted through adjusting the content and kind of oxidizer and the consumption of plasticizer. The burning rate was adjusted from 9. 3 mm/s to 11. 6 mm/s on 7. 0 MPa. The pressure exponent was dropped from 0. 61 to 0. 54.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 30 |
| 页数 | 1 |
| 期刊 | Huozhayao Xuebao/Chinese Journal of Explosives and Propellants |
| 卷 | 26 |
| 期 | 4 |
| 出版状态 | 已出版 - 2003 |
指纹
探究 'Combustion property of NEPE propellant' 的科研主题。它们共同构成独一无二的指纹。引用此
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