Vacuum Infusion Process Development for Conformal Ablative Thermal Protection System Materials
Author:
Affiliation:
1. Georgia Institute of Technology
2. University of Colorado, Boulder
3. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-5199
Reference26 articles.
1. Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System
2. Mars Science Laboratory Heatshield Development, Implementation, and Lessons Learned
3. Stardust Sample Return Capsule Design Experience
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