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

Tsunemi Hiroshi; Katayama Haruyoshi; Kimura Masashi; Daikyuji Arata; Miyaguchi Kazuhisa; Maeda Kentaro

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

机译：ISS上MAXI / SSC的在轨性能

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Wereportherethein-orbitperformanceoftheCCDcamera(MAXI/SSC)onboardtheInternationalSpaceStation(ISS).Itwascommissionedin2009August.Thisisthefirstall-skysurveymissionemployingX-rayCCDs.Itconsistsof32CCDs,eachofwhichis1inchsquare.Itisaslitcamerawithafieldofviewof1$$^circ!!!.$$5$$ imes$$90$$^circ$$,andscanstheskyastherotationoftheISS.TheCCDontheSSCiscooleddowntotheworkingtemperaturearound$$-$$60$$^circ$$Cbythecombinationofapeltiercooler,aloopheatpipeandaradiator.ThestandardobservationmodeoftheCCDisinaparallelsummode(64-binning).TheCCDfunctionsproperly,althoughitsuffersanedgeglowwhentheSunisnearthefieldofview(FOV),whichreducestheobservationefficiencyoftheSSCdowntoabout30%.TheperformanceoftheCCDiscontinuouslymonitoredbothbytheMn-KX-raysandbytheCu-KX-rays.Therearemanysourcesdetected,notonlypointsources,butextendedsources.Duetothelackofaneffectiveobservationtime,weneedmoreobservationtimetoobtainanextendedemissionanalysisextractionprocess.

机译：我们在这里报道了国际空间站（ISS）上CCD相机（MAXI / SSC）的在轨性能。该相机于2009年8月投入使用。这是采用X射线CCD的首个全天候飞行测量。它由32 CCD组成，每个都是1英寸见方的。Iisaslit相机的视野为$$$$$，大约有$$$$$范围，大约有$ 5 $$ ^ $。 TheCCDontheSSCiscooleddowntotheworkingtemperaturearound $$ - $$ 60 $$ ^ CIRC $$ Cbythecombinationofapeltiercooler，aloopheatpipeandaradiator.ThestandardobservationmodeoftheCCDisinaparallelsummode（64合并）.TheCCDfunctionsproperly，althoughitsuffersanedgeglowwhentheSunisnearthefieldofview（FOV），whichreducestheobservationefficiencyoftheSSCdowntoabout30％.TheperformanceoftheCCDiscontinuouslymonitoredbothbytheMn-KX-raysandbytheCu-KX-rays.Therearemanysourcesdetected，notonlypointsources，butextendedsources.Duetothelackofaneffectiveobservationtime ，希望有更多的观察时间来获得延长的排放分析提取过程。

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《PASJ: Publications of the Astronomical Society of Japan》 |2010年第6期|共页
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Tsunemi Hiroshi; Katayama Haruyoshi; Kimura Masashi; Daikyuji Arata; Miyaguchi Kazuhisa; Maeda Kentaro;
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1. In-orbit performance of the MAXI/SSC onboard the ISS [J] . Tsunemi H., Tomida H., Katayama H., PASJ: Publications of the Astronomical Society of Japan . 2010,第6期

机译：ISS上MAXI / SSC的在轨性能
2. In-orbit performance of MAXI gas slit camera (GSC) on ISS [J] . Sugizaki M., Mihara T., Serino M., PASJ: Publications of the Astronomical Society of Japan . 2011,第S3期

机译：ISS上MAXI气隙照相机（GSC）的在轨性能
3. In-Orbit Performance of MAXI Gas Slit Camera (GSC) on ISS [J] . Sugizaki Mutsumi, Mihara Tatehiro, Serino Motoko, PASJ: Publications of the Astronomical Society of Japan . 2011,第sp3期

机译：ISS上MAXI气隙照相机（GSC）的在轨性能
4. Solid-state slit camera (SSC) onboard MAXI [C] . Masashi KiMURA, Hiroshi Tsunemi, Hiroshi Tomida, Conference on space telescopes and instrumentation . 2010

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5. In-Orbit Performance of the CanX-2 Nanosatellite's GPS Receiver. [D] . Kahr, Erin. 2011

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6. The stretch-shortening cycle (SSC) revisited: residual force enhancement contributes to increased performance during fast SSCs of human m. adductor pollicis [O] . Wolfgang Seiberl, Geoffrey A Power, Walter Herzog, 2015

机译：重新讨论了缩短拉伸周期（SSC）：残余力的增加有助于在人类m快速SSC期间提高性能。内收肌
7. In-Orbit Performance of MAXI Gas Slit Camera (GSC) on ISS [O] . Mutsumi Sugizaki, Tatehiro Mihara, Motoko Serino, 2016

机译：Iss上maXI气体狭缝摄像机（GsC）的在轨性能

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

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