Cover Image

Stress and thermal analysis of CubeSat structure

Link to publisher's homepage at http://www.ttp.net/

Saved in:
Bibliographic Details
Main Authors: Nur Athirah, Matnawi, Mohd Afendi, Rojan, Dr., Ku Hafizan, Nasrul Amri, Mohd Amin, Dr., Mohd Shukry, Abdul Majid, Dr.
Other Authors: nurathirah.matnawi@gmail.com
Format: Article
Language:English
Published: Trans Tech Publications 2014
Subjects:
CubeSat
ANSYS
Stress
Thermal
Online Access:http://dspace.unimap.edu.my:80/dspace/handle/123456789/35102
Tags: Add Tag
No Tags, Be the first to tag this record!
id my.unimap-35102
record_format dspace
spelling my.unimap-351022014-06-05T03:33:11Z Stress and thermal analysis of CubeSat structure Nur Athirah, Matnawi Mohd Afendi, Rojan, Dr. Ku Hafizan Nasrul Amri, Mohd Amin, Dr. Mohd Shukry, Abdul Majid, Dr. nurathirah.matnawi@gmail.com afendirojan@unimap.edu.my kuhafizan769@gmail.com nasrulamri.mohdamin@unimap.edu.my shukry@unimap.edu.my CubeSat ANSYS Stress Thermal Link to publisher's homepage at http://www.ttp.net/ This paper presents the stress and thermal analysis on the CubeSat structure to study the survivability of the CubeSat during the launching process or operating condition at the orbit is presented. Various design of mechanical structures were analyzed to determine the best design for different mission requirements. Analysis on the temperature of the batteries will be conducted as it is one of the most critical components that must operate in the required temperature to avoid failure of the CubeSat. ANSYS 13.0 was used to simulate both the structural and thermal analysis. Static structural was used to study the impact of G-force on the CubeSat during the launching process and Icepak was used to study the internal temperature. All of the result will be compiled in the table and comparisons were made among different designs to determine the advantages and disadvantages of each design. Results from simulation such as: safety factor, weight, internal available space and battery discharge rate were analyzed. From the findings, there is no best design in the CubeSat structure but only the most suitable design for the mission purposes. Battery discharge rate will play an important role to determine the requirement of heater in CubeSat. 2014-06-05T03:33:11Z 2014-06-05T03:33:11Z 2014-06 Article Applied Mechanics and Materials, vol. 554, 2014, pages 426-430 1660-9336 http://www.scientific.net/AMM.554.426 http://dspace.unimap.edu.my:80/dspace/handle/123456789/35102 10.4028/www.scientific.net/AMM.554.426 en Trans Tech Publications
institution Universiti Malaysia Perlis
building UniMAP Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaysia Perlis
content_source UniMAP Library Digital Repository
url_provider http://dspace.unimap.edu.my/
language English
topic CubeSat
ANSYS
Stress
Thermal
spellingShingle CubeSat
ANSYS
Stress
Thermal
Nur Athirah, Matnawi
Mohd Afendi, Rojan, Dr.
Ku Hafizan
Nasrul Amri, Mohd Amin, Dr.
Mohd Shukry, Abdul Majid, Dr.
Stress and thermal analysis of CubeSat structure
description Link to publisher's homepage at http://www.ttp.net/
author2 nurathirah.matnawi@gmail.com
author_facet nurathirah.matnawi@gmail.com
Nur Athirah, Matnawi
Mohd Afendi, Rojan, Dr.
Ku Hafizan
Nasrul Amri, Mohd Amin, Dr.
Mohd Shukry, Abdul Majid, Dr.
format Article
author Nur Athirah, Matnawi
Mohd Afendi, Rojan, Dr.
Ku Hafizan
Nasrul Amri, Mohd Amin, Dr.
Mohd Shukry, Abdul Majid, Dr.
author_sort Nur Athirah, Matnawi
title Stress and thermal analysis of CubeSat structure
title_short Stress and thermal analysis of CubeSat structure
title_full Stress and thermal analysis of CubeSat structure
title_fullStr Stress and thermal analysis of CubeSat structure
title_full_unstemmed Stress and thermal analysis of CubeSat structure
title_sort stress and thermal analysis of cubesat structure
publisher Trans Tech Publications
publishDate 2014
url http://dspace.unimap.edu.my:80/dspace/handle/123456789/35102
_version_ 1643797706098868224
score 13.214268

Similar Items