Multidisciplinary Design Optimization of the Shape and Trajectory of a Reentry Vehicle.
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/45/147/45_147_10/_pdf
Reference19 articles.
1. Problem Formulation for Multidisciplinary Optimization
2. Technology and Operational Considerations for Low-Heat-Rate Entry Trajectories
3. Thermal Protection System Weight Minimization for the Space Shuttle through Trajectory Optimization
4. Lifting entry vehicle mass reduction through integrated thermostructural/trajectory design
5. Minimum Heating Entry Trajectories for Reusable Launch Vehicles
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