PDF下载 分享
[1]陈颖.提高试车台配气系统减压器工作可靠性的措施[J].火箭推进,2005,31(05):63-66.
 Chen Ying.Reliability improvement measures for test stand gas supplying system[J].Journal of Rocket Propulsion,2005,31(05):63-66.
点击复制

提高试车台配气系统减压器工作可靠性的措施

相似文献/References:

[1]王一白,陆星宇,李 波,等.喷管分离流动模态转换过程壁压测量试验[J].火箭推进,2015,41(05):101.
 WANG Yibai,LU Xingyu,LI Bo,et al.Test of wall pressure during transition of flow separation modes in nozzle[J].Journal of Rocket Propulsion,2015,41(05):101.
[2]刘海丽,张立强,李学华,等.低比转速高速泵螺壳形式对性能影响分析[J].火箭推进,2015,41(03):52.
 LIU Hai-li,ZHANG Li-qiang,LI Xue-hua,et al.Influence of volute case type for low-specific-speed pump on pump performance[J].Journal of Rocket Propulsion,2015,41(05):52.
[3]刘海娃.一种姿控动力装置热防护研究[J].火箭推进,2014,40(05):37.
 LIU Hai-wa.Investigation of thermal protection for attitude control propulsion device[J].Journal of Rocket Propulsion,2014,40(05):37.
[4]李志勋,田健江,张彤.姿控发动机试验热流参数测量系统设计[J].火箭推进,2010,36(02):53.
 Li Zhixun,Tian Jianjiang,Zhang Tong.Design of heat flux measurement system of attitude control engine tests[J].Journal of Rocket Propulsion,2010,36(05):53.
[5]张增亭.金属膜片贮箱膜片的数值仿真与试验验证[J].火箭推进,2009,35(03):26.
 Zhang Zengting.Numerical simulation and test veritication ot diaphragm for metal diaphragm tank[J].Journal of Rocket Propulsion,2009,35(05):26.
[6]郑丽,李清廉,罗泽明,等.减压器开启过程内部流场的 动态仿真和特性研究[J].火箭推进,2009,35(01):36.
 Zheng Li,Li Qinglian,Luo Zeming,et al.Simulation of transient flow field and dynamic characterlstlcs o士pressure reducing valve during start-up[J].Journal of Rocket Propulsion,2009,35(05):36.
[7]郑丽,李清廉,沈赤兵.大流量气体减压器响应特性的仿真研究[J].火箭推进,2008,34(02):18.
 Zheng Li,Li Qinglian,Shen Chibing.Analysis on responding characteristics of large flux pressure reducing valve[J].Journal of Rocket Propulsion,2008,34(05):18.
[8]蒋瑜.王秋红.发动机试车控制软件工程化及质量管理[J].火箭推进,2008,34(04):60.
 Jiang Yui Wang Qiuhong.Approach for improving reliability of rocket engine test control software[J].Journal of Rocket Propulsion,2008,34(05):60.
[9]陈锦.泵水力试验测控系统故障模式分析[J].火箭推进,2006,32(02):46.
 Chen Jin.Analysis of malfunction mode of measure and control system for pump hydraulic test[J].Journal of Rocket Propulsion,2006,32(05):46.
[10]李伟民.液氧/煤油发动机试验起动过程推进剂供应技术[J].火箭推进,2006,32(03):56.
 Li Weimin.Technology of propellant supply in starting of LOX/kerosene engine testing[J].Journal of Rocket Propulsion,2006,32(05):56.

更新日期/Last Update: 1900-01-01