Finite element analysis of large rocket launcher

DOI

10.2991/fmsmt-17.2017.223How to use a DOI?

Keywords

Rocket launcher structure; Finite element analysis; ANSYS

Abstract

By taking a certain type of rocket launcher structure as the research object, its loading analysis was carried out. By applying the ANSYS as a tool and by combining a typical working condition to carry out finite element analysis (FEA), the deformation and the stress values under the work condition were obtained, and the rocket launcher's strength and rigidity were analyzed. The results show that the research is based on the application of finite element software ANSYS calculation method on the launch pad is feasible, cost savings at the same time, the calculation result of finite element analysis can provide a theoretical basis for the subsequent upgrading of equipment.

Copyright

© 2017, 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  - Biao Deng
AU  - Yuan Guo
AU  - An Zhang
AU  - Sheng-jin Tang
PY  - 2017/04
DA  - 2017/04
TI  - Finite element analysis of large rocket launcher
BT  - Proceedings of the 2017 5th International Conference on Frontiers of Manufacturing Science and Measuring Technology (FMSMT 2017)
PB  - Atlantis Press
SP  - 1132
EP  - 1139
SN  - 2352-5401
UR  - https://doi.org/10.2991/fmsmt-17.2017.223
DO  - 10.2991/fmsmt-17.2017.223
ID  - Deng2017/04
ER  -