Design of Tokyo Tech nano-satellite Cute-1.7+APD II and its operation

Hiroki Ashida; Kota Fujihashi; Shinichi Inagawa; Yoshiyuki Miura; Kuniyuki Omagari; Naoki Miyashita; Saburo Matunaga; Takahiro Toizumi; Jun Kataoka; Nobuyuki Kawai

doi:10.1016/j.actaastro.2009.10.035

Design of Tokyo Tech nano-satellite Cute-1.7+APD II and its operation

Hiroki Ashida^*, Kota Fujihashi, Shinichi Inagawa, Yoshiyuki Miura, Kuniyuki Omagari, Naoki Miyashita, Saburo Matunaga, Takahiro Toizumi, Jun Kataoka, Nobuyuki Kawai

^*この研究の対応する著者

研究成果: Article › 査読

33 被引用数 (Scopus)

抄録

Cute-1.7+APD II is the 3rd satellite developed by the Laboratory for Space Systems at the Tokyo Institute of Technology. Cute-1.7+APD II is the current successor to Cute-1.7+APD. This new satellite is based on its predecessor but has some modifications to increase its reliability and robustness against radiation effects, electrical power shortage and so on. The satellite was launched by an ISRO PSLV-C9 rocket on April 28, 2008 and has operated for more than 9 months. Throughout its operation, many missions such as attitude determination and control experiments, scientific observations, photographing and communication experiments have been conducted. In this paper an overview of the Cute-1.7 series and configurations, modifications and operation results of Cute-1.7+APD II are introduced.

本文言語	English
ページ（範囲）	1412-1424
ページ数	13
ジャーナル	Acta Astronautica
巻	66
号	9-10
DOI	https://doi.org/10.1016/j.actaastro.2009.10.035
出版ステータス	Published - 2010 5
外部発表	はい

ASJC Scopus subject areas

航空宇宙工学

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10.1016/j.actaastro.2009.10.035

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title = "Design of Tokyo Tech nano-satellite Cute-1.7+APD II and its operation",

abstract = "Cute-1.7+APD II is the 3rd satellite developed by the Laboratory for Space Systems at the Tokyo Institute of Technology. Cute-1.7+APD II is the current successor to Cute-1.7+APD. This new satellite is based on its predecessor but has some modifications to increase its reliability and robustness against radiation effects, electrical power shortage and so on. The satellite was launched by an ISRO PSLV-C9 rocket on April 28, 2008 and has operated for more than 9 months. Throughout its operation, many missions such as attitude determination and control experiments, scientific observations, photographing and communication experiments have been conducted. In this paper an overview of the Cute-1.7 series and configurations, modifications and operation results of Cute-1.7+APD II are introduced.",

keywords = "Avalanche photo diode, Cute-1.7+APD II, Ground station network, Magnetic torquer, Nano-satellite",

author = "Hiroki Ashida and Kota Fujihashi and Shinichi Inagawa and Yoshiyuki Miura and Kuniyuki Omagari and Naoki Miyashita and Saburo Matunaga and Takahiro Toizumi and Jun Kataoka and Nobuyuki Kawai",

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doi = "10.1016/j.actaastro.2009.10.035",

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AU - Ashida, Hiroki

AU - Fujihashi, Kota

AU - Inagawa, Shinichi

AU - Miura, Yoshiyuki

AU - Omagari, Kuniyuki

AU - Miyashita, Naoki

AU - Matunaga, Saburo

AU - Toizumi, Takahiro

AU - Kataoka, Jun

AU - Kawai, Nobuyuki

PY - 2010/5

Y1 - 2010/5

N2 - Cute-1.7+APD II is the 3rd satellite developed by the Laboratory for Space Systems at the Tokyo Institute of Technology. Cute-1.7+APD II is the current successor to Cute-1.7+APD. This new satellite is based on its predecessor but has some modifications to increase its reliability and robustness against radiation effects, electrical power shortage and so on. The satellite was launched by an ISRO PSLV-C9 rocket on April 28, 2008 and has operated for more than 9 months. Throughout its operation, many missions such as attitude determination and control experiments, scientific observations, photographing and communication experiments have been conducted. In this paper an overview of the Cute-1.7 series and configurations, modifications and operation results of Cute-1.7+APD II are introduced.

AB - Cute-1.7+APD II is the 3rd satellite developed by the Laboratory for Space Systems at the Tokyo Institute of Technology. Cute-1.7+APD II is the current successor to Cute-1.7+APD. This new satellite is based on its predecessor but has some modifications to increase its reliability and robustness against radiation effects, electrical power shortage and so on. The satellite was launched by an ISRO PSLV-C9 rocket on April 28, 2008 and has operated for more than 9 months. Throughout its operation, many missions such as attitude determination and control experiments, scientific observations, photographing and communication experiments have been conducted. In this paper an overview of the Cute-1.7 series and configurations, modifications and operation results of Cute-1.7+APD II are introduced.

KW - Avalanche photo diode

KW - Cute-1.7+APD II

KW - Ground station network

KW - Magnetic torquer

KW - Nano-satellite

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Design of Tokyo Tech nano-satellite Cute-1.7+APD II and its operation

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