•  
  •  
 

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.

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.