1. 1) Milos, F. S.: Galileo Probe Heat Shield Ablation Experiment, J. Spacecraft Rockets, 34, 6 (1997), pp. 705-713.
2. 2) Milos, F. S., Chen, Y. K. and Brewer, R. A.: Analysis of Galileo Probe Heatshield Ablation and Temperature Data, J. Spacecraft Rockets, 36, 3 (1999), pp. 298-306.
3. 3) Kato, S., Kanno, Y., Okuyama, K., Uegaki, E., Yamada, T. and Suzuki, T.: Design and Post-Flight Analysis of REV Thermal Protection System, JAXA Research and Development Report, JAXA-RR-04-045, 2005, pp. 77-103 (in Japanese).
4. 4) Okuyama, K., Kato, S., Yamada, T. and Zako, M.: Oxidation Characteristics of the Carbonized CFRP under the Air Environments, TANSO, 213 (2004), pp. 128-133 (in Japanese).
5. 5) Tran, H., Johnson, C., Rasky, D., Hui, F., Chen, Y. K. and Hsu, M.: Phenolic Impregnated Carbon Ablators (PICA) for Discovery Missions, AIAA Paper 96-1911, 31st AIAA Thermophysics Conference, New Orleans, LA, 1996.