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.
Audu, Aminu Muhammed and Hai, Huang
"Structural Analysis and Optimization A Must in Spacecraft Projects,"
International Journal of Mechanical and Industrial Engineering: Vol. 2:
1, Article 14.
Available at: https://www.interscience.in/ijmie/vol2/iss1/14