Ablation and thermal response program for spacecraft heatshield analysis
- 12 January 1998
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Silicone impregnated reusable ceramic ablators for Mars follow-on missionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Methodology for full-body TPS sizing of Access-to-Space vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Solution strategy for thermal response of nonablating thermal protection systems at hypersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Mars Pathfinder trajectory based heating and ablation calculationsJournal of Spacecraft and Rockets, 1995
- Navier-Stokes solutions with surface catalysis for Martian atmospheric entryJournal of Spacecraft and Rockets, 1993