1. K. Fujita, T. Suzuki, and T. Ozawa, “Development of a Pilot Model of Hypersonic Rarefied Wind-Tunnel,” in 27th International Symposium on Rarefied Gas Dynamics, edited by D. A. Levin, I. J. Wysong, and A. J. Garcia, AIP Conference Proceedings, New York, 2011, vol. 1333, pp. 407–412, ISBN 978-0-7354-0889-0, Pacific Grove, CA, 10-15 July 2010.
2. Aerodynamic Measurements and Computational Analyses in Hypersonic Rarefied Flows
3. G. A. Bird, “Molecular Gas Dynamics and the Direct Simulation of Gas Flows,” in Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Clarendon, Oxford, England, U.K., 1994.
4. K. Fujita, G. Ishigami, R. Hatakenaka, M. Takai, H. Toyota, N. Ogawa, M. Haruki, H. Takeuchi, T. Nonomura, K. Yamada, H. Takayanagi, T. Ozawa, S. Matsuyama, A. Oyama, A. Yamagishi, S. Kameda, H. Miyamoto, and T. Satoh, Japan’s Mars Rover Mission - System Design & Development Status, ISTS paper 2015-k-37, Kobe, Hyogo (2015).
5. Conceptual study and key technology development for Mars Aeroflyby sample collection