System design of the Hayabusa 2—Asteroid sample return mission to 1999 JU3

Author:

Tsuda Yuichi,Yoshikawa Makoto,Abe Masanao,Minamino Hiroyuki,Nakazawa Satoru

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference5 articles.

1. Yoshikawa, M., Hayabusa-2 Project Team, Outline of the Next Asteroid Sample Return Mission of Japan: Hayaubsa-2, in: 28th International Symposium on Space Technology and Science, 2011-k-19, 2011.

2. Tsuda, Y., Ogawa, N., Morimoto, M., Kawaguchi, J., Trajectory Design of Hayabusa-2, JAXA Workshop on Astrodynamics and Flight Mechanics, A-5, Sagamihara, 2011.

3. Muller, T.G., Durech, J., Hasegawa, S., Abe, M., Kawakami, K., Kasuga, T., Kinoshita, D., Kuroda, D., Urakawa, S., Okamura, S., Sarugaku, Y., Miyasaka, S., Takagi, Y., Weissman, P.R., Choi, Y.J., Larson, S., Yanagisawa, K., Nagayama, S., Thermo-physical properties of 162173 (1999 JU3), a potential flyby and rendezvous target for interplanetary missions Acta Astronaut.525 (A145(January)) 2011.

4. Sawada, H., Tachibana, S., Okazaki, R., Okamoto C., Yano, H., The Sampling System of HAYABUSA2 Missions, in: 63rd International Astronautical Congress, IAC-12-A3.4.6, Naples, 2012.

5. Saiki, T., Imamura H., Sawada, H., Okamoto C., Development Status of Small Carry-on Impactor for Hayabusa-2 Mission, in: 63rd International Astronautical Congress, IAC-12-A3.4.8, Naples, 2012.

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