Orbit Verification Results of the De-Orbit Mechanism Demonstration CubeSat FREEDOM-Reference-Cited by-同舟云学术

Orbit Verification Results of the De-Orbit Mechanism Demonstration CubeSat FREEDOM

Published:2019 Issue:3 Volume:17 Page:295-300
ISSN:1884-0485
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
language:en
Short-container-title:AEROSPACE TECHNOLOGY JAPAN

Author:

UTO Hiroki¹,KUWAHARA Toshinori²,HONDA Tomoyuki²

Affiliation:

1. Nagoya Technical Center, Nakashimada Engineering Works, Ltd.

2. Department of Aerospace Engineering, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/17/3/17_17.295/_pdf

Reference12 articles.

1. 1) Sakamoto, Y., Tanabe, Y., Yagisawa, H., Sugimura, N., Yoshida, K., Nishio, M., Nakajo, T. and Akiyama, H.: Operation Results of Cubesat RAIKO Released from International Space Station, Trans. JSASS, Aerospace Tech. Japan, 12, ists29 (2014), pp.Tf_7-Tf_12.

2. 2) Kuwahara, T., Sakamoto, Y., Yoshida, K., Takahashi, Y., Fukuhara, T. and Kurihara, J.: Mission and System of the Earth Observation Microsatellite RISING-2, Proceedings of 8th Symposium on Small Satellites for Earth Observation, Berlin, April 4–8, 2011.

3. 3) Mogi, T., Kuwahara, T. and Uto, H.: Structural Design of De-orbit Mechanism Demonstration CubeSat FREEDOM, Trans. JSASS, Aerospace Tech. Japan, 14, ists30 (2016), pp.Pf_61-Pf_68.

4. 4) Akagi, H., Takata, M., Watanabe, H. and Oikawa, K.: Kibo's contribution to broadening the possibilities for Micro/Nano-satellite, Proceedings of the SpaceOps 2016 Conference, Daejeon, Korea, May 16-20, 2016, AIAA 2016-2517.

5. 5) Uto, H., Kuwahara, T. and Mogi, T.: Specifications of Thin Film Deployment Type De-orbit Device DOM1500, 4th UNISEC-Global Meeting, Deorbit Device Competition, Varna, Bulgaria, 2016.

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