Preliminary Study on De-Orbiting Large-Scale Debris Using a Charged Membrane in Low Earth Orbit

Author:

MURANAKA Takanobu1,NAGATA Takuma1,NAGAI Hiroki1,UENO Kazuma1,OKUMURA Teppei2,OHKAWA Yasushi2

Affiliation:

1. Department of Electrical and Electronic Engineering, Chukyo University

2. Research and Development Directorate, Japan Aerospace Exploration Agency

Publisher

Japan Society for Aeronautical and Space Sciences

Reference8 articles.

1. 1) Ley, W., Wittmann, K., and Hallmann, W.: Handbook of Space Technology, A John Wiley and Sons, Ltd., Publication, West Sussex, 2009, pp. 100–113.

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

3. 3) Liou, J. C.: An Active Debris Removal Parametric Study for LEO Environment Remediation, Advances in Space Research, 47 (2011), pp. 1865–1876.

4. 4) Ohkawa, Y., Kawamoto, S., Matsumoto, K., Shiomi, H., and Kitamura, S.: R&D of Electrodynamic Tether for On-orbit Demonstration, 5th Space Debris Workshop, Tokyo, Japan, JAXA-SP-13-018, 2014.

5. 5) JAXA-SP-13-018, 2014. Kawamoto, S.: Status of Space Debris Removal Research, Bulletin of The Society of Japanese Aerospace Companies “Aerospace” , 741 (2015), pp. 5–11 (in Japanese).

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