Development of the Mars Science Laboratory Heatshield Thermal Protection System
- 14 June 2009
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Development of a High-Fidelity Thermal/Ablation Response Model for SLA-561VPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Numerical Simulations of Protruding Gapfillers on the Mars Science Laboratory HeatshieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Aerothermodynamic Design of the Mars Science Laboratory HeatshieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection SystemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection SystemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon AblatorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2009
- Post-Flight Analysis of the Stardust Sample Return Capsule Earth EntryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2008
- 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
- Mars Pathfinder Heatshield Design and Flight ExperienceJournal of Spacecraft and Rockets, 1999