1. 1) Tran, H., Johnson, C., Rasky, D., Hui, F., Chen, Y. K., and Hsu, M.: Phenolic Impregnated Carbon Ablators (PICA) for Discovery Class Missions, NASA TM 110440, 1996.
2. 2) Wright, M. J., Beck, R. A. S., Edquist, K. T., Driver, D., Sepka, S. A., Slimko, E. M., Willcockson, W. H., DeCaro, A., and Hwang, H. H.: Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System, AIAA Paper 2009-4231, 2009.
3. 3) Suzuki, T., Aoki, T., Ogasawara, T., and Fujita, K.: Nonablative Lightweight Thermal Protection System for Mars Aeroflyby Sample Collection Mission, Acta Astronautica, 136 (2017), pp. 407–420.
4. 4) Fujita, K., Suzuki, T., Ozawa, T., Sakai, T., Dantsuka, Y., Ishida, Y., and Watanabe, Y.: Ablation Sensor Unit for Flight Demonstration on HTV Small Recovery Capsule, AIAA Paper 2017-0899, 2017.
5. 5) Nouri, N., Panerai, F., Tagavi, K. A., Mansour, N. N., and Martin, A.: Evaluation of the Anisotropic Radiative Conductivity of a Low-density Carbon Fiber Material from Realistic Microscale Imaging, Int. J. Heat Mass Transfer, 95 (2016), pp. 535–539.