航天推进技术研究院主办
[1]李进华,雷 永,王乃娟.一种测试带压条件下MON-1饱和蒸汽压的新方法[J].火箭推进,2013,39(02):63-66.
LI Jin-hua,LEI Yong,WANG Nai-juan.New method to test bubble point pressure of MON-1 under pressure condition[J].Journal of Rocket Propulsion,2013,39(02):63-66.
点击复制
LI Jin-hua,LEI Yong,WANG Nai-juan.New method to test bubble point pressure of MON-1 under pressure condition[J].Journal of Rocket Propulsion,2013,39(02):63-66.
一种测试带压条件下MON-1饱和蒸汽压的新方法
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
39
期数:
2013年02期
页码:
63-66
栏目:
研究与设计
出版日期:
2013-04-30
- Title:
- New method to test bubble point pressure of MON-1 under pressure condition
- 文章编号:
- 1672-9374(2013)02-0079-04
- Keywords:
- MON-1; saturated vapor pressure; testing method
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 为了解决采用一般方法不能测定带压条件下液体物质饱和蒸汽压的难题，研究、开发出一种新的测试方法。设计、加工了试验装置，实测得到一定温度和压力条件下MON-1的饱和蒸汽压值，并与拟合方程计算值和相关文献数据进行比较，结果表明该测试方法可行、精确、可靠。
- Abstract:
- In order to resolve the problem that common methods cannot test bubble point pressure of liquid substance under pressure condition, a new testing method was studied and developed, and an experimental equipment for testing the bubble point pressure of MON-1 in different temperature was fabricated. The saturated vapor pressure value was obtained under the certain conditions of temperature and pressure. It was compared with literature data and the calculated value obtained by fitted equation. The result indicates that the new testing method is feasible, accurate and credible.
参考文献/References:
[1]李亚裕. 液体推进剂[M]. 北京: 宇航出版社, 2011.
[2]才满瑞, 王向阳, 刘兴武, 等. 国外航天运载器的发展状况、发展趋势及采用的关键技术[J]. 导弹与航天运载技术, 1998 (3): 16－18.
[3]庞建国, 刘小平, 邵永平, 等. 推进剂加注后末修贮箱压力变化机理[J]. 火箭推进, 2005, 31(5): 15-17.
[4]陈阳, 张振鹏, 瞿骞, 等. 液体火箭发动机试验台贮箱增压系统数值仿真[J]. 航空动力学报, 2007, 22(1): 96-101.
[5]李进华, 孙兆懿. 四氧化二氮胶体的饱和蒸气压测试及分析[J]. 火炸药学报, 2007, 30(1): 74－77.
[6]PONNER S S. The chemistry of propellants[M]. London: Pergamen Prees, 1960.
[7]SMITH I D. The determination of the helium saturation level of monomethyl hydrazine and MON-3 nitrogen tetroxide, NASA-TM-101262 [R]. USA: NASA-TM, 1979.
[8]潘玉竹, 余永刚, 张琦. AF-315液体单元推进剂高压燃速的实验研究[J]. 弹道学报, 2012, (2): 79-82.
[9]李健, 周文禄. 推力室气动加热及结构传热耦合分析[J].导弹与航天运载技术, 2012, (3): 18-22.
[10]李青, 王天舒, 马兴瑞. 充液航天器液体晃动和液固耦合动力学的研究与应用[J]. 力学进展, 2012, (4): 472-481.
[11]TIM Edwards. Liquid fuels and propellants for aerospace propulsion:1903～2003. Journal of Propulsion and Power, 2003, 19(6): 28-32.
[12]AMES D L, TURNER D W. The static method studies on the vapor pressure of dinitrogen tetroxide and dinitrogen pentoxide[J]. Physical and Chemical Sciences, 1976, 348(1653): 89-94.
备注/Memo
收稿日期：2012-09-１8；修回日期：2012-11-23
基金项目：中国航天科技集团公司支撑项目（2011JY01）
作者简介：李进华（1980—），男，高级工程师，研究领域为新型液体推进剂
更新日期/Last Update:
1900-01-01