|Table of Contents|

Design of floating coupling for on-orbit resupply(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2011年04期
Page:
45-49
Research Field:
研究与设计
Publishing date:

Info

Title:
Design of floating coupling for on-orbit resupply
Author(s):
MA Hai-tao CHEN Jian WEI Qing TANG Mei-fang
Shanghai Institute of Space Propulsion, Shanghai 200233, China
Keywords:
on-orbit resupply floating coupling transfer
PACS:
V43-34
DOI:
-
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.

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.

Memo

Memo:
-
Last Update: 1900-01-01