航天推进技术研究院主办
[1]马海涛,陈 健,魏 青,等.一种在轨补加用浮动断接器设计[J].火箭推进,2011,37(04):45-49.
MA Hai-tao,CHEN Jian,WEI Qing,et al.Design of floating coupling for on-orbit resupply[J].Journal of Rocket Propulsion,2011,37(04):45-49.
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MA Hai-tao,CHEN Jian,WEI Qing,et al.Design of floating coupling for on-orbit resupply[J].Journal of Rocket Propulsion,2011,37(04):45-49.
一种在轨补加用浮动断接器设计
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
37
期数:
2011年04期
页码:
45-49
栏目:
研究与设计
出版日期:
2011-08-15
- Title:
- Design of floating coupling for on-orbit resupply
- 文章编号:
- 1672-9374(2011)04-0045-05
- Keywords:
- on-orbit resupply; floating coupling; transfer
- 分类号:
- V43-34
- 文献标志码:
- A
- 摘要:
- 对国外的在轨补加用浮动断接器的研究进展进行了总结，在此基础上，提出了一种在轨补加用浮动断接器的设计方案。通过对浮动断接器方案的选择和初步设计，确定了其工作方式、关键技术及解决途径，并进行了初步的原理验证和性能检测。结果表明，浮动断接器原理可行，方案合理，通过进一步的结构优化，可应用于在轨补加。
- Abstract:
- The research evolution of floating coupling on board used in on-orbit resupply is summarized, based on which a design scheme of floating coupling used in on-orbit resupply is proposed. The working mode, key technique and solutions were determined by selection of schemes and design of the prototype. The scheme was verified and performances of the prototype were tested. The result shows that the design of the floating coupling is reasonable and suitable for on-orbit resupply.
参考文献/References:
[1]HAMILTON W. Automatic refueling coupling for on-orbit spacecraft servicing, AIAA89-2731[R]. USA:AIAA, 1989.
[2]STUDENICK R M. Automated fluid interface system (AFIS) for remote satellite refueling, AIAA 90-1884[R]. USA: AIAA, 1990.
[3]CARDIN J. A standardized spacecraft resupply interface, AIAA 91-1841[R]. USA: AIAA, 1991.
[4]刘国强. ANSOFT工程电磁场有限元分析[M]. 北京: 电子工业出版社, 2005.
[5] D K 休泽耳著. 赵元修, 吴守生, 金如山, 等译. 液体推进剂火箭发动机设计[M]. 北京: 国防工业出版社, 1973.
[6] 刘国球. 液体火箭发动机原理[M]. 北京: 宇航出版社, 1993.
[7] R H 沃林著. 宋学义, 张正义译.密封件与密封件手册[M]. 北京: 国防工业出版社, 1990.
[8] 朱宁昌. 液体火箭发动机设计（下）[M]. 北京: 宇航出版社,1994.
相似文献/References:
[1]刘海娃,汤建华.浮动断接器热控设计与仿真[J].火箭推进,2015,41(01):23.
LIU Hai-wa,TANG Jian-hua.Design and simulation of thermal control for floating coupling[J].Journal of Rocket Propulsion,2015,41(04):23.
备注/Memo
收稿日期：2010-10-13；修回日期：2010-12-14
作者简介： 马海涛（1979—），男，工程师，研究领域为液体火箭发动机阀门设计
更新日期/Last Update:
1900-01-01