低温阀在液体火箭发动机试验中的应用
被引量:3
Cryogenic Valve for Liquid Rocket Engine Application
摘要
介绍了低温阀在国内外液体火箭发动机试验中的应用情况,分析了我国低温阀在航天领域的研究现状,提出了低温阀的研究方向。
出处
《火箭推进》
CAS
2004年第1期32-37,共6页
Journal of Rocket Propulsion
参考文献2
-
1[2]Horstmann M, Langel G. Dasa Cryogenic Valves and Future Development Options. AIAA98-3203, 34th AIAA/ASME/ASEE Joint Propulsion Conference Exhibit, Cleveband, OH, Julyl3-15, 1998.
-
2[3]Salerno L J. A Cryogenic Valve for Spacecraft Applications. AIAA 82-0077, 20thAIAA Aerospace Sciences Meeting, Orlando, Florida, Jan.11-14, 1982.
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-
1魏超,吴维,林硕,苑士华.一种高速脉冲阀动态特性[J].机械工程学报,2011,47(6):138-142. 被引量:10
-
2戴佳,黄敏超,余勇,朱恒伟,马加庆.电磁阀动态响应特性仿真研究[J].火箭推进,2007,33(1):40-48. 被引量:60
-
3程亚威,李小明,陈维宇.液氧主阀的方案及设计[J].火箭推进,2007,33(2):17-19. 被引量:5
-
4LIU Song,YAO Bin.Adaptive robust control of programmable valves with manufacturer supplied flow mapping only[C]//The 43rd IEEE Conference on Decision and Control.Nassau:IEEE,2004:1117-1122.
-
5RAO Z,BONE G M.Nonlinear modeling and control of servo pneumatic actuators control systems technology[J].IEEE Transactions on Control System Technology,2008,16(3):562-569.
-
6CAVALLO P A,HOSANGADI A,AHUJA V.Transient simulations of valve motion in cryogenic systems[C]// Proceedings of the 35th AIAA Fluid Dynamics Conference and Exhibit.USA:American Institute of Aeronautics and Astronautics,2009:1-10.
-
7LIU Kun,ZHANG Yu-lin.A study on versatile simulation of liquid propellant rocket engine systems transients,AIAA 2000-3771[R].USA:AIAA,2000.
-
8BOSNYATSKIJ G P,BARINUD V B,PARSADANOV G M,et al.Optimization of inter-relations of manmachine-external environment-reserve of reliability of system[J].Gazovaya Promyshlennost,2001 (12):35-40.
-
9龙升照.钱学森与人机环境系统工程[C]//第八届中国人机环境系统工程大会.深圳:[出版者不详],2007.
-
10MA L H,YAN H Z.Comprehensive evaluation of fully mechanized mining face security based on unascertrained-Information entropy model[C]// Proceedings of the 2nd IEEE International Conference on Computer Science and Information Technology.Beijing,China:IEEE,2009:268-271.
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