Preliminary System Design of Small Lunar Landing Demonstrator SLIM-Reference-Cited by-同舟云学术

Preliminary System Design of Small Lunar Landing Demonstrator SLIM

Published:2018 Issue:0 Volume:17 Page:35-43
ISSN:1884-0477
Container-title:AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Author:

SAWAI Shujiro¹,FUKUDA Seisuke¹,SAKAI Shinichiro¹,KUSHIKI Kenichi¹,ARAKAWA Tetsuhito¹,SATO Eiichi¹,TOMIKI Atsushi¹,MICHIGAMI Keisuke¹,KAWANO Taro¹,OKAZAKI Shun¹,KUKITA Akio¹,MIYAZAWA Yu¹,UEDA Satoshi¹,TOBE Hirobumi¹,MARU Yusuke¹,SHIMOJI Haruhiko²,SHIMIZU Yasuhiro²,SHIBASAKI Yusuke²,SHIMADA Sadanori²,YOKOI Takahiro³,YABUSHITA Takeshi³,SATO Kenichiro³,NAKAMURA Kazuyuki⁴,KUHARA Takahiro⁴,TAKAMI Tsuyoshi⁵,TANAKA Nobuhiko⁵,FURUKAWA Katsumi⁵

Affiliation:

1. ISAS / JAXA

2. Mitsubishi Electric Corporation

3. Mitsubishi Space Software Co., Ltd.

4. Technosolver Corporation

5. Mitsubishi Heavy Industries, Ltd.

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/astj/17/0/17_JSASS-D-16-00050/_pdf

Reference9 articles.

1. 2) Nakaya, K., Fukuda, S., Sakai, S., Yamazaki, A., Uemizu, K., Toriumi, T., Takahashi, J., Maehara, M., Okahashi, T., and Sawai, S.: Development of Flexible Standard Bus for ISAS/JAXA Small Scientific Satellite Series, Trans. JSASS Aerospace Technology Japan, 10, ists28 (2012), pp. Tf_5-Tf_9.

2. 4) European Cooperation for Space Standardization: SpaceWire - Links, Nodes, Routers and Networks, Issue 2, 2008, ECSS-E50-12C.

3. 6) Saito, H., Hirahara, H., Mizuno, T., Fukuda, S., Fukushima, Y., Asamura, et al. : Small satellite REIMEI for auroral observations, Acta Astronautica, 69, 7-8(2011), pp.499-513.

4. 8) Ishii, N., Nakamura, M., Imamura, T., Abe, T., Kimura, M., and Ohshima, T. : System Analysis and Orbit Design for PLANET-C Venus Climate Orbiter, 27th International Symposium on Space Technology and Science (ISTS), 2009-k-53p, 2009.

5. 9) Ishii, N., Yamakawa, H., Sawai, S., Shida, M., Hashimoto, T., Nakamura, M., Imamura, T., Abe, T., Oyama, K., and Nakatani, I. : Current Status of the PLANET-C Venus Orbiter Design, Advances in Space Research, 34, 8(2004), pp.1668-1672.

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