In-Orbit Performance of the MAXI/SSC onboard the ISS

被引:39
|
作者
Tsunemi, Hiroshi [1 ]
Tomida, Hiroshi [2 ]
Katayama, Haruyoshi [3 ]
Kimura, Masashi [1 ]
Daikyuji, Arata [4 ]
Miyaguchi, Kazuhisa [5 ]
Maeda, Kentaro [5 ]
机构
[1] Osaka Univ, Grad Sch Sci, Dept Earth & Space Sci, Osaka 5600043, Japan
[2] JAXA, ISAS, ISS Sci Project Off, Tsukuba, Ibaraki 3058505, Japan
[3] JAXA, Earth Observat Res Ctr, Tsukuba, Ibaraki 3058505, Japan
[4] Miyazaki Univ, Fac Engn, Dept Appl Phys, Miyazaki 8892192, Japan
[5] Hamamatsu Photon KK, Div Solid State, Hamamatsu, Shizuoka 4358558, Japan
关键词
instrumentation: detectors; space vehicles: instruments; X-ray CCDs; CHARGE-COUPLED-DEVICE; PROTON IRRADIATION EXPERIMENT; INTERNATIONAL-SPACE-STATION; IMAGE MISSION ONBOARD; X-RAY ASTRONOMY; XMM-NEWTON; CCD CAMERA; INJECTION; MONITOR;
D O I
10.1093/pasj/62.6.1371
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
We report here the in-orbit performance of the CCD camera (MAXI/SSC) onboard the International Space Station (ISS). It was commissioned in 2009 August. This is the first all-sky survey mission employing X-ray CCDs. It consists of 32 CCDs, each of which is I inch square. It is a slit camera with a field of view of 1.degrees 5 x 90 degrees, and scans the sky as the rotation of the ISS. The CCD on the SSC is cooled down to the working temperature around -60 degrees C by the combination of a peltier cooler, a loop heat pipe and a radiator. The standard observation mode of the CCD is in a parallel sum mode (64-binning). The CCD functions properly, although it suffers an edge glow when the Sun is near the field of view (FOV), which reduces the observation efficiency of the SSC down to about 30%. The performance of the CCD is continuously monitored both by the Mn-K X-rays and by the Cu-K X-rays. There are many sources detected, not only point sources, but extended sources. Due to the lack of an effective observation time, we need more observation time to obtain an extended emission analysis extraction process.
引用
收藏
页码:1371 / 1379
页数:9
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