Affiliation:
1. ESI-ATE
2. ESI CFD, Inc.
3. Alabama A&M University
Publisher
American Institute of Aeronautics and Astronautics
Reference13 articles.
1. 2Chen, Y. K., Henline, W. D., and Tauber, M. E. "Trajectory Based Heating and Ablation Calculation for Mars PathfinderAeroshell.JournalofSpacecraftandRockets,Vol.32,1995.
2. 4Olynick,D.R."AerothermodynamicsoftheStardustSampleReturnCapsule,"AIAAPaper1998-0167,1998.
3. 5Olynick, D. R., Chen, Y. K., and Tauber, M. "Forebody TPS sizing with radiation and ablation for the Stardust samplereturncapsule,"AIAAPaper1997-2474,1997.