《Table 4Aging program condition》
提示：宽带有限、当前游客访问压缩模式
本系列图表出处文件名：随高清版一同展现
《"Effects of Plasticizers,Antioxidants and Burning Rate Modifiers on Aging Performance of the HTPB/HMDI Composite Solid Propellant"》
Therefore，due to the presence and the growth of these micro‐fractures along the service life of the solid rocket propellants can cause cohesive critical cracks take place during the ignition phase，these cracks increased the area of the burning surface lead to an out‐of‐design state.To study these phenomena，the aging program developed in was applied to eval‐uate the aging mechanisms involved in the accelerat‐ed aging program at 70℃for 90 d.The relation be‐tween the normal and accelerated aging program is represented in Table 4 and given in detail in the pa‐per of Bohn[14].
| 图表编号 | XD0033899900 严禁用于非法目的 |
|---|---|
| 绘制时间 | 2019.01.25 |
| 作者 | Ahmed M Enew、Ehab Abadir、Sahar Elmarsafy、Karim K Elsharkawy |
| 绘制单位 | Chemical Department,Faculty of Engineering,Cairo University、Chemical Department,Faculty of Engineering,Cairo University、Chemical Department,Faculty of Engineering,Cairo University、School of Chemistry and Environment,Beijing University of Aeronautics and A |
| 更多格式 | 高清、无水印（增值服务） |
