Multi-level of Fidelity Multi-Disciplinary Design Optimization of Small, Solid-Propellant Launch Vehicles-Reference-Cited by-同舟云学术

Multi-level of Fidelity Multi-Disciplinary Design Optimization of Small, Solid-Propellant Launch Vehicles

Published:2010 Issue:180 Volume:53 Page:73-83
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

ROSHANIAN Jafar¹,JODEI Jahangir¹,MIRSHAMS Mehran¹,EBRAHIMI Reza¹,MIRZAEE Masood¹

Affiliation:

1. MDO Laboratory, Department of Aerospace and Mechanical Engineering, K.N. Toosi University of Technology

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/53/180/53_180_73/_pdf

Reference38 articles.

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2. 2) Zhao, Y., Chen, X. and Wang, Z.: SIDE: A Tool for Integrated Multidisciplinary Design Optimization of Spacecrafts, AIAA Paper 2006-7119, 2006.

3. 3) Jian, G., et al.: A Distributed Multidisciplinary Design Optimization Architecture for Spacecraft Design, AIAA Paper 2002-5481, 2002.

4. 4) McAllister, C. D., et al.: Multidisciplinary Design Optimization Testbed Based on Autonomous Under Water Vehicle Design, AIAA Paper 2002-5630, 2002.

5. 5) Fitzgerald, C. J., et al.: A Conceptual Design Environment for Technology Selection and Performance Optimization for Torpedoes, AIAA Paper 2002-5590, 2002.

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