Quantitative Assessment of Multidisciplinary Design Models for Expendable Launch Vehicles-Reference-Cited by-同舟云学术

Quantitative Assessment of Multidisciplinary Design Models for Expendable Launch Vehicles

Published:2014-01 Issue:1 Volume:51 Page:343-359
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Castellini Francesco,Lavagna Michèle R.,Riccardi Annalisa,Büskens Christof

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32527

Reference37 articles.

1. Design Methodologies for Space Transportation Systems

2. AIAA Technical Committee on Multidisciplinary Design Optimization, “White Paper on Current State of the Art,” AIAA, Washington, D.C., Dec. 1991.

3. Sobieszczanski-SobieskiJ. “Multidisciplinary Optimization for Engineering Systems: Achievements and Potential,” NASA TM-101566, March 1989.

4. Multidisciplinary Design and Optimization of the Silent Aircraft

5. OldsJ. R. “Multidisciplinary Design Techniques Applied to Conceptual Aerospace Vehicle Design,” Ph.D. Thesis, North Carolina State Univ., Raleigh, NC, 1993.

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