Research on the Design Method of Modular Structure for Satellites

DOI

10.2991/mems.2012.59How to use a DOI?

Keywords

Modularization; truss structure; ball joints

Abstract

In order to achieve rapid injection of micro-nano satellites, based on the analysis of latest related research result, a conception that truss structure is applied to the modular structure design of micro-nano satellite is presented, and a detailed approach using ball joint and rod as load-carrying structure and its specific design examples are given. The result shows that the truss structure can realize the standardization of the mechanical interface to complete the modular structure design of the micro-nano satellites.

Copyright

© 2012, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - SONG Wei-Xu
AU  - ZHANG Ke-ke
AU  - LI Chun-Peng
AU  - SU Rui-Feng
PY  - 2012/12
DA  - 2012/12
TI  - Research on the Design Method of Modular Structure for Satellites
BT  - Proceedings of the 1st International Conference on Mechanical Engineering and Material Science (MEMS 2012)
PB  - Atlantis Press
SP  - 219
EP  - 221
SN  - 1951-6851
UR  - https://doi.org/10.2991/mems.2012.59
DO  - 10.2991/mems.2012.59
ID  - Wei-Xu2012/12
ER  -