1. Identification of Docking Possibility Criteria including Recovery from Incomplete Grasping of Docking Mechanism for Nanosatellite
2. (2) Ashida, H., Nishida, J., Omagari, K., Fujiwara, K., Konda, Y., Yamanaka, T., Tanaka, Y., Maeno, M., Fujihashi, K., Inagawa, S., Miura, Y., And Matunaga, S., Flight Model Development of Tokyo Tech Nano-Satellite Cute-1.7 + APD II, Transactions of Space Technology Japan, Vol. 7, (2009), pp.Tf_37-Tf_42.
3. (3) Nakaya, K., Konoue, K., Sawada, H., Ui, K., Okada, H., Miyashita, N., Iai, M., Urabe, T., Yamaguchi, N., Kashiwa, M., Omagari, K., Morita, I., and Matunaga, S., Tokyo Tech CubeSat: CUTE-I - Design & Development of Flight Model and Future Plan -, AIAA 21st International Communications Satellite Systems Conference and Exhibit, AIAA 2003-2388, Yokohama, Japan (2003).
4. (4) Iai, M., Sawada, H., Nakaya, K., Ui, K., Miyashita, N., Kashiwa, M., Yamaguchi, N., and Matunaga, S., Orbital Data Analysis of Picosatellite CUTE-I, 24th International Symposium on Space Technology and Science, Miyazaki, June 1-6, (2004), 2004-f-08.
5. The Hinode X-Ray Telescope (XRT): Camera Design, Performance and Operations