航天推进技术研究院主办
[1]刘瑞敏,卜玉,孙德,等.新一代运载火箭动力系统试车总体试验技术研究[J].火箭推进,2017,43(01):72-77.
LIU Ruimin,BU Yu,SUN De,et al.Research on overall test technology of power system for a new generation launch vehicle[J].Journal of Rocket Propulsion,2017,43(01):72-77.
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LIU Ruimin,BU Yu,SUN De,et al.Research on overall test technology of power system for a new generation launch vehicle[J].Journal of Rocket Propulsion,2017,43(01):72-77.
新一代运载火箭动力系统试车总体试验技术研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
43
期数:
2017年01期
页码:
72-77
栏目:
测控与试验
出版日期:
2017-04-01
- Title:
- Research on overall test technology of power system for a new generation launch vehicle
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 针对动力系统试验规模大、风险高、密度高、并行环节多、技术难度大等突出特点,试验主体承担单位细化落实试验主体抓总责任,充分发挥抓总、策划、牵引能力,注重工艺流程的持续优化、加强试验过程的统筹协调、安全防范和风险管控,统一指挥十余个参试系统,统领近十个参试单位形成的试验队有序工作,技术状态控制有效,确保了三型运载火箭八个模块十二次动力系统试车准时准点和圆满成功,为三型运载火箭按期首飞奠定了基础.
- Abstract:
- The power system test is a large-scale project,and has some outstanding features,such as high risk,high density,many parallel links and high difficulty.Therefore,the main undertaking unit of the test detailed its main responsibility,giving full play to its overall grasping,planning and leading capacities,focusing on continuous optimization of the technological process,strengthening the co-ordination,security and risk control in the test process,commanding the test system with more than ten parameters in unison,and guiding the ten test participation units to work together orderly to ensure that the twelve tests for eight modules of the Third-model Launch Vehicle successfully.On the basis of this,the foundation for the on-time first launch of the new generation launch vehicle was laid.
参考文献/References:
[1]卜玉, 刘瑞敏, 梁怀喜. 新一代运载火箭氢氧模块动力系统试验风险分析[J]. 火箭推进, 2016 (2): 66-70.
BU Yu, LIU Ruimin, LIANG Huaixi. Risk analysis of LOX/LH2 module power system test for a new generation launch vehicle[J]. Journal of rocket propulsion, 2016(2): 66-70.
[2]朱耀龙, 李护林. 液体火箭发动机工艺与过程关键特性研究[J]. 火箭推进, 2014(12): 64-73.
ZHU Yaolong, LI Hulin. Research on key features of liquid rocket engine manufacturing technique and process [J]. Journal of rocket propulsion, 2014(12): 64-73.
[3]肖瑾,赵雯.导弹型号总体设计工作流管理技术研究[J]. 华北航天工业学院学报, 2006(4): 6-8.
[4]尚志,敬铮.首次空间交会对接项目管理创新实践[J]. 中央企业项目管理创新技能大赛优秀案例, 2012(6): 29-33.
[5]杨前进, 张立伟. 航天型号AIT精细化管理模式研究[J].管理与实践, 2016(1): 22-25.
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SONG Jingjing,GUO Jing,WANG Haifeng,et al.Optimal design on gas inflation system of power system test stand[J].Journal of Rocket Propulsion,2016,42(01):73.
[3]卜玉,刘瑞敏,梁怀喜,等.新一代运载火箭氢氧模块动力系统试验风险分析[J].火箭推进,2016,42(01):66.
BU Yu,LIU Ruimin,LIANG Huaixi,et al.Risk analysis of LOX/LH2 module power system test for a new generation launch vehicle[J].Journal of Rocket Propulsion,2016,42(01):66.
备注/Memo
收稿日期：2016-07-29；修回日期：2016-09-07 基金项目：航天支撑技术项目（617010403） 作者简介：刘瑞敏（1983—），女，研究员，研究领域为火箭发动机试验技术
更新日期/Last Update:
1900-01-01