摘要
NEPE propellant is a new kind of solid propellant developed in the 1980s containing blend nitrate ester plasticized polyether adhesive. By NEPE propellant high temperature accelerated aging test (NEPE propellants were prematurely aged at 55, 60, 65, 70, 75, and 80?) and mechanical performance test,this paper found the characterization of propellant aging characteristics, found the deficiencies and inapplicability of existing two life prediction methods (the prediction method based on the dynamic mechanical properties test and life prediction based on Berthlot equation), and then through improved Berthlot model estimated propellant storage life.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | 51st AIAA/SAE/ASEE Joint Propulsion Conference |
| 出版商 | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN（印刷版） | 9781624103216 |
| DOI | |
| 出版状态 | 已出版 - 2015 |
| 活动 | 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015 - Orlando, 美国 期限: 27 7月 2015 → 29 7月 2015 |
出版系列
| 姓名 | 51st AIAA/SAE/ASEE Joint Propulsion Conference |
|---|
会议
| 会议 | 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015 |
|---|---|
| 国家/地区 | 美国 |
| 市 | Orlando |
| 时期 | 27/07/15 → 29/07/15 |
指纹
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Xiong, Y., Sui, X., & Wang, N. (2015). Research on NEPE propellant life prediction model. 在 51st AIAA/SAE/ASEE Joint Propulsion Conference (51st AIAA/SAE/ASEE Joint Propulsion Conference). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2015-3872