•  
  •  
 

International Journal of Mechanical and Industrial Engineering

Abstract

An efficient weight reduction and improved stiffness requirements of a practical spacecraft Trainsat-1 satellite are presented, utilizing abound high efficient method used in MSC. Nastran. Numerical example was also given to test the validity of the software in spacecraft application.

DOI

10.47893/IJMIE.2012.1069

Share

COinS
 
 

To view the content in your browser, please download Adobe Reader or, alternately,
you may Download the file to your hard drive.

NOTE: The latest versions of Adobe Reader do not support viewing PDF files within Firefox on Mac OS and if you are using a modern (Intel) Mac, there is no official plugin for viewing PDF files within the browser window.