DocumentCode
2045529
Title
Design analysis & verification of separation test platform for spacecraft
Author
Zheng Shengyu ; Yi Wangmin ; Feng Wei ; Guo Dabao ; Chen Qiwei ; Tang Laiying ; Fang Zhikai ; Li Qing
Author_Institution
Beijing Inst. of Spacecraft Environ. Eng., Beijing, China
fYear
2015
fDate
2-5 Aug. 2015
Firstpage
1636
Lastpage
1641
Abstract
The spacecraft which is composed by several modules should be tested on the ground whether the modules can be separated successfully or not, and separation locomotion data should be obtained as well. This paper has described the requirements and difficulties of separation test, and has designed the zero gravity platform. The critical design parameters are obtained by the analysis result of MSC.ADAMS software. It can be concluded that the platform is correctly designed through verification of the prototype.
Keywords
aerospace computing; aerospace testing; space vehicles; MSC.ADAMS software; separation locomotion data; separation test platform; spacecraft; zero gravity platform; Acceleration; Friction; Gravity; Space vehicles; Springs; Wheels; ADAMS; separation test; simulation equipment; spacecraft; zero gravity;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2015 IEEE International Conference on
Conference_Location
Beijing
Print_ISBN
978-1-4799-7097-1
Type
conf
DOI
10.1109/ICMA.2015.7237730
Filename
7237730
Link To Document