Proton Irradiation Experiment for X-ray Charge-Coupled Devices of the Monitor of All-Sky X-ray Image Mission Onboard the International Space Station: II. Degradation of Dark Current and Identification of Electron Trap Level
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概要
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We have investigated the radiation damage effects on a charge-coupled device (CCD) to be used for the Japanese X-ray mission, the monitor of all-sky X-ray image (MAXI), onboard the international space station (ISS). A temperature dependence of the dark current as a function of incremental dose is studied. We found that the protons having energy of ${>}292$ keV seriously increased the dark current of the devices. In order to improve the radiation tolerance of the devices, we have developed various device architectures to minimize the radiation damage in orbit. Among them, nitride oxide enables us to reduce the dark current significantly and therefore we adopted nitride oxide for the flight devices. We also compared the dark current of a device in operation and that out of operation during the proton irradiation. The dark current of the device in operation became twofold that out of operation, and we thus determined that devices would be turned off during the passage of the radiation belt. The temperature dependence of the dark current enables us to determine the electron trap level that generates the dark current. We fitted dark current as a function of temperature by the thoretical models and found that the dark current increase after proton irradiations is caused by, at least, two kinds of electron trap levels. The shallow trap level ($E_{\text{c}}-E_{\text{t}} < 0.2$ eV where $E_{\text{c}}$ and $E_{\text{t}}$ are the energy at the bottom of the conduction band and the energy level of electron trap) might be associated with oxygen which is dominant at the operating temprature of ${>}210$ K. On the other hand, another trap level is located roughly at the center of the silicon bandgap which might be associated with divacancies or P–V traps. We finally investigated the spatial distribution of the low-energy protons in the orbit of the ISS. Their density has a peak around $l \sim 20{{\degree}}$ and $b \sim -55{{\degree}}$ independent of the altitude. The peak value is roughly two orders of magnitude higher than that at the South Atlantic Anomaly.
- 2003-07-15
著者
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Miyata Emi
Department Of Earth And Space Science Graduate School Of Science Osaka University
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Tsunemi Hiroshi
Department Of Earth And Space Science Graduate School Of Science Osaka University
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KOUNO Hirohiko
Department of Earth & Space Science, Graduate School of Science, Osaka University
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KAMIYAMA Daisuke
Department of Earth & Space Science, Graduate School of Science, Osaka University
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KAMAZUKA Tomoyuki
Department of Earth & Space Science, Graduate School of Science, Osaka University
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TOMIDA Hiroshi
National Space Development Agency of Japan (NASDA), Tsukuba Space Center
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Matsuta Kensaku
Department Of Physics Tokyo University Of Science
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Minamisono Tadanori
Department Of Physics And Laboratory Of Nuclear Studies Faculty Of Science Osaka University
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Mihara Mototsugu
Department Of Physics Graduate School Of Science Osaka University
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Fukuda Mitsunori
Department Of Molecular Neurobiology Institute Of Medical Science University Of Tokyo
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Miyaguchi Kazuhisa
Solid State Division Hamamatsu Photonics K. K.
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Tomida Hiroshi
National Space Development Agency of Japan (NASDA), Tsukuba Space Center, 2-1-1 Sengen Tsukuba Ibaragi 305-8505, Japan
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TSUNEMI Hiroshi
Department of Astrophysics, Faculty of Science, Osaka University
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Matsuta Kensaku
Department of Physics, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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Fukuda Mitsunori
Department of Physics, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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Tsunemi Hiroshi
Department of Earth & Space Science, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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Mihara Mototsugu
Department of Physics, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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Kamazuka Tomoyuki
Department of Earth & Space Science, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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Minamisono Tadanori
Department of Physics, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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Kouno Hirohiko
Department of Earth & Space Science, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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MIYATA Emi
Department of Astrophysics, Faculty of Science, Osaka University
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Miyata Emi
Department of Earth & Space Science, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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Kamiyama Daisuke
Department of Earth & Space Science, Graduate School of Science, Osaka University, 1-1 Machikaneyama-cho, Toyonaka, Osaka 560-0043, Japan
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