著者
Tamagawa Toru Hayato Asami Nakamura Satoshi TERADA Yukikatsu BAMBA Aya HIRAGA Junko S. HUGHES John P. HWANG Una KATAOKA Jun KINUGASA Kenzo KUNIEDA Hideyo TANAKA Takaaki TSUNEMI Hiroshi UENO Masaru HOLT Stephen S. KOKUBUN Motohide MIYATA Emi SZYMKOWIAK Andrew TAKAHASHI Tadayuki TAMURA Keisuke UENO Daisuke MAKISHIMA Kazuo
出版者
社団法人日本天文学会
雑誌
PASJ : publications of the Astronomical Society of Japan (ISSN:00046264)
巻号頁・発行日
vol.61, no.1, pp.S167-S174, 2009-01-30

Tycho's supernova remnant was observed by the XIS and HXD instruments onboard the Suzaku satellite on 2006 June 26-29 for 92 ks. The spectrum up to 30 keV was well fitted with a two-component model, consisting of a power-law with photon index of 2.7 and a thermal bremsstrahlung model with temperature of 4.7 keV. The former component can alternatively be modeled as synchrotron emission from a population of relativistic electrons with an estimated roll-off energy of around 1 keV. In the XIS spectra, in addition to the prominent Fe K_alpha line (6.445 keV), we observe for the first time significant K_alpha line emission from the trace species Cr and Mn at energies of 5.48 keV and 5.95 keV, respectively. Faint K_beta lines from Ca (4.56 keV) and Fe (7.11 keV) are also seen. The ionization states of Cr and Mn, based on their line centroids, are estimated to be similar to that of Fe K_alpha (Fe XV or XVI).
著者
Miyata Emi Kouno Hirohiko Kamiyama Daisuke Kamazuka Tomoyuki Mihara Mototsugu Fukuda Mitsunori Matsuta Kensaku Tsunemi Hiroshi Minamisono Tadanori Tomida Hiroshi Miyaguchi Kazuhisa
出版者
Published by the Japan Society of Applied Physics through the Institute of Pure and Applied Physics
雑誌
Japanese journal of applied physics. Pt. 1, Regular papers & short notes (ISSN:00214922)
巻号頁・発行日
vol.42, no.7, pp.4564-4570, 2003-07-15
参考文献数
18
被引用文献数
5

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.