Stagewise Multidisciplinary Design Optimization Formulation for Optimal Design of Expendable Launch Vehicles
Author:
Affiliation:
1. Centre National d ’ Etudes Spatiales, 75612 Paris, France
2. ONERA – The French Aerospace Lab, 91123 Palaiseau, France
3. IRCCyN, 44321 Nantes, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.52507
Reference27 articles.
1. Design Optimization of a Space Launch Vehicle Using a Genetic Algorithm
2. Multi-disciplinary Analysis and Optimisation Approach for the Design of Expendable Launchers
3. Optimal Conceptual Design of Two-Stage Reusable Rocket Vehicles Including Trajectory Optimization
4. Decomposition approach to solving the All-up trajectory optimizationproblem
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