1. F.S. Milos, Y.-K. Chen, W.M. Gongdon, and J.M. Thornton, “Mars Pathfinder Entry Temperature Data, Aerothermal Heating, and Heatshield Material Response,” J. Spacecraft Rockets 36, 380 (1999).
2. D. Paterna, R. Monti, R. Savino, and A. Esposito, “Experimental and Numerical Investigation of Martian Atmosphere Entry,” J. Spacecraft Rockets 39, 227 (2002).
3. N.E. Afonina and V.G. Gromov, “Investigation of the Flow in the Deceleration Region during Spacecraft Entry in the Martian Atmosphere on the Basis of a Viscous Shock Layer Model” [in Russian], Institute of Mechanics of Moscow State University, Preprint No. 31-97 (1997).
4. S.T. Surzhikov, “2D CFD/RGD Model of Space Vehicles,” in: Proc. 1st Int. Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 8–10 October 2003, Lisbon, Portugal, ESA-533 (2003), p. 95.
5. S.T. Surzhikov, “Numerical Simulation of Heat Radiation Generated by Entering Space Vehicle,” AIAA Paper No. 2379 (2004).