Assessment of collision risk to electrodynamic tether used for de-orbiting

A. Oishi, Hiroshi Hirayama, Toshiya Hanada, T. Yasaka, C. Pardini, L. Anselmo

研究成果: 会議への寄与タイプ論文

3 引用 (Scopus)

抄録

An electrodynamic tether has been recently proposed as an alternative solution to remove spent upper stages and satellites from low Earth orbit. The electrodynamic tether is also subjected to orbital debris and meteoroids collisions, however. In addition, the collision risk on such tethers would be more serious than that on spacecraft. The collision risk on tether is great due to the very large collision cross sectional area, and because of the small diameter, tether has high risk of severing by collisions of relatively small orbital debris and meteoroids. Risk of the orbital debris collisions on the tether was studied in Kyushu University (Japan) and ISTI/CNR (Italy). These two studies used different techniques to evaluate the collision risk. We evaluate the severing risk of tether and the survivability of tether during the de-orbiting from LEO by each technique.

元の言語英語
ページ4065-4071
ページ数7
出版物ステータス出版済み - 12 1 2004
イベントInternational Astronautical Federation - 55th International Astronautical Congress 2004 - Vancouver, カナダ
継続期間: 10 4 200410 8 2004

その他

その他International Astronautical Federation - 55th International Astronautical Congress 2004
カナダ
Vancouver
期間10/4/0410/8/04

Fingerprint

electrodynamics
Electrodynamics
collision
Tetherlines
collisions
Debris
debris
meteoroids
low Earth orbits
orbitals
Spacecraft
Italy
Orbits
Earth (planet)
Japan
Satellites
spacecraft

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

これを引用

Oishi, A., Hirayama, H., Hanada, T., Yasaka, T., Pardini, C., & Anselmo, L. (2004). Assessment of collision risk to electrodynamic tether used for de-orbiting. 4065-4071. 論文発表場所 International Astronautical Federation - 55th International Astronautical Congress 2004, Vancouver, カナダ.

Assessment of collision risk to electrodynamic tether used for de-orbiting. / Oishi, A.; Hirayama, Hiroshi; Hanada, Toshiya; Yasaka, T.; Pardini, C.; Anselmo, L.

2004. 4065-4071 論文発表場所 International Astronautical Federation - 55th International Astronautical Congress 2004, Vancouver, カナダ.

研究成果: 会議への寄与タイプ論文

Oishi, A, Hirayama, H, Hanada, T, Yasaka, T, Pardini, C & Anselmo, L 2004, 'Assessment of collision risk to electrodynamic tether used for de-orbiting', 論文発表場所 International Astronautical Federation - 55th International Astronautical Congress 2004, Vancouver, カナダ, 10/4/04 - 10/8/04 pp. 4065-4071.
Oishi A, Hirayama H, Hanada T, Yasaka T, Pardini C, Anselmo L. Assessment of collision risk to electrodynamic tether used for de-orbiting. 2004. 論文発表場所 International Astronautical Federation - 55th International Astronautical Congress 2004, Vancouver, カナダ.
Oishi, A. ; Hirayama, Hiroshi ; Hanada, Toshiya ; Yasaka, T. ; Pardini, C. ; Anselmo, L. / Assessment of collision risk to electrodynamic tether used for de-orbiting. 論文発表場所 International Astronautical Federation - 55th International Astronautical Congress 2004, Vancouver, カナダ.7 p.
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AU - Oishi, A.

AU - Hirayama, Hiroshi

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AU - Anselmo, L.

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