| 固体推进剂燃烧波温度分布测定 |
| |
| 引用本文： | 张杰.固体推进剂燃烧波温度分布测定[J].固体火箭技术,2005,28(3):228-231. |
| |
| 作者姓名： | 张杰 |
| |
| 作者单位： | 清华大学核能与新能源技术研究院,北京,100084 |
| |
| 摘 要： | 采用相对光强度法测定了双基推进剂、复合推进剂及NEPE（氧化剂为HNIW或HMX）推进剂的燃烧火焰温度分布。结果表明，用相对光强度法测得推进剂的最高燃烧火焰温度比热电偶法更接近推进剂的理论燃烧温度，测试压强越高，最高燃烧火焰温度与理论燃烧火焰温度的误差越小。
|
| 关 键 词： | 固体推进剂 燃烧 温度分布 |
| 文章编号： | 1006-2793（2005）03-0228-04 |
| 收稿时间： | 2005-03-29 |
| 修稿时间： | 2005-04-19 |
Temperature distribution measurement of combustion wave for solid propellant |
| |
| ZHANG Jie.Temperature distribution measurement of combustion wave for solid propellant[J].Journal of Solid Rocket Technology,2005,28(3):228-231. |
| |
| Authors: | ZHANG Jie |
| |
| Abstract: | Temperature distribution of combustion flame of double base propellant,composite propellant and NEPE propellant(taking HNIW or HMX as oxidizer)were measured by using relative light intensity method.The results show that the highest combustion flame temperature measured by relative light intensity method is much closer to theoretical combustion flame temperature than that measured by thermocouple method.The higher measured pressure is,the lower error between the highest combustion flame temperature and theoretical combustion flame temperature is. |
| |
| Keywords: | solid propellant combustion temperature distribution |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
