CIVILICA We Respect the Science
Publisher of Iranian Journals and Conference Proceedings
Paper
title

Multidisciplinary design optimization of a reentry spacecraft

Credit to Download: 0 | Page Numbers 4 | Abstract Views: 31
Year: 2020
COI code: ISME28_254
Paper Language: English

How to Download This Paper

For Downloading the Fulltext of CIVILICA papers please visit the orginal Persian Section of website.

Authors Multidisciplinary design optimization of a reentry spacecraft

Masoud Kabganian - Ryerson University /Aerospace Engineering, Toronto, Canada;
  Jafar Roshanian - K. N. Toosi University of Technology/Aerospace Engineering, Tehran, Iran;
  Masoud Ebrahimi - Tarbiat Modares University/Mechanical Engineering, Tehran, Iran;

Abstract:

In the present paper, after studying several articles in this area and studying research on reentry vehicle or manned spacecraft, it can be seen that optimizing even one discipline or subsystem from this vehicle without regard to other discipline is practically impossible. Therefore, in most research in this area, we can see the multidisciplinary optimization footprint or multi-objective optimization.Multidisciplinary design optimization (MDO) focuses on the use of numerical optimization in the design of systems with a number of subsystems or disciplines. The main reason for using MDO in multidisciplinary designs is that the performance of the system is related not only to the act of each individual disciplines but also to their interactions. With the help of MDO in the early stage of the design process, one can simultaneously enhance the design and decrease the time and cost of the entire design cycle.In conclusion, considering various methods and research works, in a combined and innovative method, the multidisciplinary design optimization of a reentry spacecraft or a space capsule was implemented, with considering variables, constraints and various parameters applied in several geometric shapes with suggested dimensions for a reentry spacecraft [1].

Keywords:

Optimization Design, Multidisciplinary, Spacecraft, Reentry to earth, Space Capsule

Perma Link

https://www.civilica.com/Paper-ISME28-ISME28_254.html
COI code: ISME28_254

how to cite to this paper:

If you want to refer to this article in your research, you can easily use the following in the resources and references section:
Kabganian, Masoud; Jafar Roshanian & Masoud Ebrahimi, 2020, Multidisciplinary design optimization of a reentry spacecraft, 28th Annual Conference of Mechanical Engineering, تهران - دانشگاه صنعتي امير كبير, انجمن مهندسان مكانيك ايران, https://www.civilica.com/Paper-ISME28-ISME28_254.htmlInside the text, wherever referred to or an achievement of this article is mentioned, after mentioning the article, inside the parental, the following specifications are written.
First Time: (Kabganian, Masoud; Jafar Roshanian & Masoud Ebrahimi, 2020)
Second and more: (Kabganian; Roshanian & Ebrahimi, 2020)
For a complete overview of how to citation please review the following CIVILICA Guide (Citation)

Research Info Management

Export Citation info of this paper to research management softwares

New Related Papers

Iran Scientific Advertisment Netword

Share this paper

WHAT IS COI?

COI is a national code dedicated to all Iranian Conference and Journal Papers. the COI of each paper can be verified online.