Multiobjective Optimization of Earth-Entry Vehicle Heat Shields
Author:
Affiliation:
1. University of Maryland, University of Maryland
2. University of Colorado, Boulder, Colorado 80309
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.42565
Reference46 articles.
1. Entry System Options for Human Return from the Moon and Mars
2. Space Vehicle Design, Second Edition
3. Apollo entry aerodynamics.
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