1. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
2. Wright, M.J., Beck, R.A.S., Edquist, K.T., Driver, D., Sepka, S., Slimko, E., Willcockson, B., DeCaro, T., and Hwang, H.H. "Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System," AIAA Paper No. 2009-4xxx,June2009.
3. Dec, J. A. and Mitcheltree, R. A. "Probabilistic Design of A Mars Sample Return Entry Vehicle Thermal Protection System," AIAA paper 2002-0910.