Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator
- 1 September 2010
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 47 (5), 786-805
- https://doi.org/10.2514/1.42949
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- Two-Dimensional Ablation, Thermal Response, and Sizing Program for Pyrolyzing AblatorsJournal of Spacecraft and Rockets, 2009
- Development of the Mars Science Laboratory Heatshield Thermal Protection SystemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Two-Dimensional Ablation and Thermal Response Analyses for Mars Science Laboratory HeatshieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Erratum on "Erratum on 'Performance of a Low Density Ablative Heat Shield Material'"Journal of Spacecraft and Rockets, 2008
- Erratum on "Performance of a Low Density Ablative Heat Shield Material"Journal of Spacecraft and Rockets, 2008
- Two-Dimensional Implicit Thermal Response and Ablation Program for Charring MaterialsJournal of Spacecraft and Rockets, 2001
- Ablation and Thermal Response Program for Spacecraft Heatshield AnalysisJournal of Spacecraft and Rockets, 1999
- Stardust Sample Return Capsule Design ExperienceJournal of Spacecraft and Rockets, 1999
- Data-Parallel Line Relaxation Method for the Navier-Stokes EquationsAIAA Journal, 1998
- Comprehensive model for multicomponent ablation thermochemistryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997