Damage Assessment for Electrodynamic Tape Tether against Space Debris Impact-Reference-Cited by-同舟云学术

Damage Assessment for Electrodynamic Tape Tether against Space Debris Impact

Published:2021 Issue:1 Volume:19 Page:34-41
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:

FUJIWARA Michihiro¹,TOMIZAKI Honoka¹,HASEGAWA Sunao²,OHTANI Kiyonobu³,MAKIHARA Kanjuro¹³

Affiliation:

1. Department of Aerospace Engineering, Tohoku University

2. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

3. Institute of Fluid Science, Tohoku University

Publisher

Japan Society for Aeronautical and Space Sciences

Link

https://www.jstage.jst.go.jp/article/tastj/19/1/19_19.34/_pdf

Reference31 articles.

1. 1) Pelton, J. N.: Space Debris and Other Threats from Outer Space, Springer-Verlag, New York, 2013, pp. 17–44.

2. 2) National Aeronautics and Space Administration: Orbital Debris Quarterly News, NASA Orbital Debris Program Office, Vol. 21, No. 3, 2017.

3. 3) Kessler, D. J.: Collisional Cascading: The Limits of Population Growth in Low Earth Orbit, Advances in Space Research, 11 (1991), pp. 63–66.

4. 4) 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.

5. 5) Uto, H., Kuwahara, T., and Honda, T.: Orbit Verification Results of the De-orbit Mechanism Demonstration CubeSat FREEDOM, Trans. JSASS Aerospace Tech. Japan, 17 (2019), pp. 295–300.

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