| 发动机推进剂高能射线半值层试验研究 |
| |
| 引用本文： | 卢洪义,李善高,孙建国,史佩.发动机推进剂高能射线半值层试验研究[J].海军航空工程学院学报,2007,22(1):106-108. |
| |
| 作者姓名： | 卢洪义 李善高 孙建国 史佩 |
| |
| 作者单位： | 海军航空工程学院飞行器工程系,山东烟台,264001 |
| |
| 基金项目： | 总装“十五”预研课题(41328010406) |
| |
| 摘 要： | 制作了试验用的大型导弹发动机推进剂模块,选用了9MeV的电子加速器作为实验用的高能射线源,设计了推进剂半值层的试验方案,根据不同的推进剂的厚度,取得了相应的试验结果,通过分析得到科学的结论。
|
| 关 键 词： | 半值层 推进剂 电子加速器 |
| 修稿时间： | 2006年2月26日 |
The test research of high-energy X-ray HVL for SRM. Propellant |
| |
| LU Hongyi,LI Shan'gao,SUN Jianguo,SHI Pei.The test research of high-energy X-ray HVL for SRM. Propellant[J].Journal of Naval Aeronautical Engineering Institute,2007,22(1):106-108. |
| |
| Authors: | LU Hongyi LI Shan'gao SUN Jianguo SHI Pei |
| |
| Institution: | Department of Airborne Vehicle Engineering,NAEI,Yantai,Shandong,264001,Department of Airborne Vehicle Engineering,NAEI,Yantai,Shandong,264001,Department of Airborne Vehicle Engineering,NAEI,Yantai,Shandong,264001 and Department of Airborne Vehicle Engineering,NAEI,Yantai,Shandong,264001 |
| |
| Abstract: | The big SRM. Propellant module is made for testing. 9MeV electron accelerator is selected to be high energy X-ray source. Testing precept is designed to study propellant HVL. The since conclusion is got by testing result from different size propellant. |
| |
| Keywords: | HVL Propellant electron accelerator |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《海军航空工程学院学报》浏览原始摘要信息 |
| 点击此处可从《海军航空工程学院学报》下载免费的PDF全文 |
|
