| 环境温度对固体火箭发动机气密性检查影响分析 |
| |
| 引用本文： | 艾春安,李剑,王斌.环境温度对固体火箭发动机气密性检查影响分析[J].火箭推进,2006,32(3):8-11. |
| |
| 作者姓名： | 艾春安 李剑 王斌 |
| |
| 作者单位： | 第二炮兵工程学院201教研室,陕西,西安,710025 |
| |
| 摘 要： | 针对M型固体火箭发动机的具体结构,建立了其在储存环境条件下的传热模型,并进行了计算,分析了环境温度变化对“压差法”气密性检查结果的影响,验证了采用“压差法”对固体火箭发动机进行气密性检测的可靠性。
|
| 关 键 词： | 固体火箭发动机 气密性检查 温度 |
| 文章编号： | (2006)03-0008-04 |
| 收稿时间： | 2006-02-20 |
| 修稿时间： | 2006-03-16 |
Influence of ambient temperature on solid rocket motor airtight test |
| |
| Ai Chun'an,Li Jian,Wang Bin.Influence of ambient temperature on solid rocket motor airtight test[J].Journal of Rocket Propulsion,2006,32(3):8-11. |
| |
| Authors: | Ai Chun'an Li Jian Wang Bin |
| |
| Abstract: | Based on the structure of a kind of solid rocket motor, the model of heat transfer of the motor in the storage environment was given, and calculated with the method of simulation. The influence of temperature on the result of the airtight test was analyzed, and the reliability of the method of pressure discrepancy test for airtightness was validated. |
| |
| Keywords: | solid rocket motor airtight test temperature |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
