Deployment and steering dynamics of spinning solar sail "IKAROS"

Osamu Mori; Yoji Shirasawa; Yasuyuki Miyazaki; Hiraku Sakamoto; Mitsue Hasome; Nobukatsu Okuizumi; Hirotaka Sawada; Hiroshi Furuya; Saburo Matunaga; Michihiro Natori; Yuichi Tsuda; Takanao Saiki; Ryu Funase; Yuya Mimasu; Junichiro Kawaguchi

doi:10.7446/jaesa.0404.07

Deployment and steering dynamics of spinning solar sail "IKAROS"

Osamu Mori, Yoji Shirasawa, Yasuyuki Miyazaki, Hiraku Sakamoto, Mitsue Hasome, Nobukatsu Okuizumi, Hirotaka Sawada, Hiroshi Furuya, Saburo Matunaga, Michihiro Natori, Yuichi Tsuda, Takanao Saiki, Ryu Funase, Yuya Mimasu, Junichiro Kawaguchi

研究成果: Article › 査読

6 被引用数 (Scopus)

抄録

The Japan Aerospace Exploration Agency (JAXA) makes the world's first solar power sail craft IKAROS demonstration of photon propulsion and thin film solar power generation during its interplanetary cruise. The spacecraft deploys and spans a membrane of 20 meters in diameter using the spin centrifugal force. It also deploys thin film solar cells on the membrane, in order to evaluate its thermal control property and anti-radiation performance in the real operational field. The spacecraft weighs approximately 310kg, launched together with the agency's Venus Climate Orbiter, AKATSUKI on May 21, 2010. This paper presents the summary of development and operation of IKAROS.

本文言語	English
ページ（範囲）	79-96
ページ数	18
ジャーナル	Journal of Aerospace Engineering, Sciences and Applications
巻	4
号	4
DOI	https://doi.org/10.7446/jaesa.0404.07
出版ステータス	Published - 2012 10月
外部発表	はい

ASJC Scopus subject areas

航空宇宙工学

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10.7446/jaesa.0404.07

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引用スタイル

Mori, O., Shirasawa, Y., Miyazaki, Y., Sakamoto, H., Hasome, M., Okuizumi, N., Sawada, H., Furuya, H., Matunaga, S., Natori, M., Tsuda, Y., Saiki, T., Funase, R., Mimasu, Y., & Kawaguchi, J. (2012). Deployment and steering dynamics of spinning solar sail "IKAROS". Journal of Aerospace Engineering, Sciences and Applications, 4(4), 79-96. https://doi.org/10.7446/jaesa.0404.07

Mori, O, Shirasawa, Y, Miyazaki, Y, Sakamoto, H, Hasome, M, Okuizumi, N, Sawada, H, Furuya, H, Matunaga, S, Natori, M, Tsuda, Y, Saiki, T, Funase, R, Mimasu, Y & Kawaguchi, J 2012, 'Deployment and steering dynamics of spinning solar sail "IKAROS"', Journal of Aerospace Engineering, Sciences and Applications, vol. 4, no. 4, pp. 79-96. https://doi.org/10.7446/jaesa.0404.07

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AU - Miyazaki, Yasuyuki

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AU - Hasome, Mitsue

AU - Okuizumi, Nobukatsu

AU - Sawada, Hirotaka

AU - Furuya, Hiroshi

AU - Matunaga, Saburo

AU - Natori, Michihiro

AU - Tsuda, Yuichi

AU - Saiki, Takanao

AU - Funase, Ryu

AU - Mimasu, Yuya

AU - Kawaguchi, Junichiro

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AB - The Japan Aerospace Exploration Agency (JAXA) makes the world's first solar power sail craft IKAROS demonstration of photon propulsion and thin film solar power generation during its interplanetary cruise. The spacecraft deploys and spans a membrane of 20 meters in diameter using the spin centrifugal force. It also deploys thin film solar cells on the membrane, in order to evaluate its thermal control property and anti-radiation performance in the real operational field. The spacecraft weighs approximately 310kg, launched together with the agency's Venus Climate Orbiter, AKATSUKI on May 21, 2010. This paper presents the summary of development and operation of IKAROS.

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KW - Membrane

KW - Solar sail

KW - Steering

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Deployment and steering dynamics of spinning solar sail "IKAROS"

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