TY  - RPRT
TI  - Structural Evaluation and Optimization of Aeroshell Design Properties for Launch and Reentry Load Cases for Future AI-Informed Design Leveraging Large Datasets
AU  - John Bell
AU  - Sasan Armand
AU  - Jamshid Samareh
UR  - https://ntrs.nasa.gov/citations/20230008057
ID  - 20230008057
ER  -