Aerothermodynamic Optimization of Reentry Heat Shield Shapes for a Crew Exploration Vehicle
Author:
Affiliation:
1. University of Maryland, College Park, Maryland 20742
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.27219
Reference23 articles.
1. Aerodynamic Behavior of the Viking Entry Vehicle: Ground Test and Flight Results
2. Theoretical method for calculating aerodynamic characteristics of spherically blunted cones
3. Aerodynamic Stability of Reentry Heat Shield Shapes for a Crew Exploration Vehicle
4. A generic geometric transformation that unifies a wide range of natural and abstract shapes
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