euv spectroscopic observation of jupiter’s inner magnetosphere...
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EUV spectroscopic observation of Jupiter’s inner magnetosphere 極端紫外分光による木星内部磁気圏の観測的研究. 2009 年 11 月 25 日 宇宙研 STP セミナー 東大吉川研 / 吉岡和夫. Contents. General introduction Jupiter and Io plasma torus (Target) Spectral diagnosis using EUV emissions (Approach) - PowerPoint PPT PresentationTRANSCRIPT
PowerPoint Presentation
EUV spectroscopic observation of Jupiters inner magnetosphere
20091125STP/ContentsGeneral introductionJupiter and Io plasma torus (Target)Spectral diagnosis using EUV emissions (Approach)
Analysis of the data obtained by CASSINI/UVIS during its Jupiter flybyThe principle and method of the spectral diagnosisThe evaluation of the plasma parameters around the Io torusHot electron ratioAnother parameters
Development of the EUV spectroscope on board the earth-orbiting satelliteInstrumental overviewEntrance mirrorGratingDetectorMicrochannel plate with photocathodeResistive anode encoderThe shield structure and noise evaluationThe feasibility study of the observation for the Io torus
Summary
Future works271500 km6400 km9h55min24 h*420,000 nT31,000 nT5.1 AU**1 AU* ** 1 AU = 1.5E+8 km ~ 2000 RJ 5 ~ 8RJ
NASA/NEW HORIZONS
NASA/CASSINI333
57 km/s
~ 100 eV5 eV
EUV10%Pick up energyEUV radiation~ 2 TWIonsS+, S++, S3+, S4+, O+, O++
Core electrons: ~5 eV, ~2000 ele./cc
Fast neutralTransport444
3S+, S++, S3+590%EUVIonsS+, S++, S3+, S4+, O+, O++
Core electrons: ~5 eV, ~2000 ele./cc
Galileo>1 keVFrank and Paterson, 2000()Pick up Pick up energyEUV radiation~ 2 TWHot electronsEUVFast neutralTransport
661
24680, 701, 822, 1077
7--EIS~0.06A FWHMXIIIS/N
Watanabe et al. 2009
203.8 A202.0 A [cm-3][cm-3]89
Nj NJ
Thermally averaged cross sectionA-valueNJCHIANTISII, SIII, SIV, SV, OII, OIII
11
CASSINI/UVISCASSINI1997NASAUVISCASSINIEUV (560 ~ 1180)20 mm 20 mm
200010
100030S/N5.5~6.5RJ
Esposito et al. 199912
SV/SIII=0.00, OIII/SIII=0.21 keV2OII/SIIISVEUV1OIII:Voyager-1OIIIOII2OIIOIII1SII/SIII131SIV/SIII
13
S/NVS
10DUSKDAWN15
15
Voyager -1Sitteler and Strobel, 1987
Voyager-1Baganel 1994Distance from Jupiter center (RJ)
163216C2 = 15 vs 18
vs
vs OII/SIII
219 vs vs SII/SIII vs SIV/SIII vs SII/SIII vs OII/SIII vs SIV/SIII
320OII/OIII vs SII/SIII vs SII/SIII vs SIV/SIII vs OII/SIII
OII/OIII vs SIV/SIIISII/OIII vs SIV/SIII
2100 ~ 2700 [cm-3]
3.55 ~ 4.55 [eV]
2.7 ~ 4.3 [%]
OII / SIII: 0.96 ~ 1.40
SII/SIII: 0.31 ~ 0.42
SIV/SIII: 0.14 ~ 0.19
21160 eV1keV
EUV60
EUV
23ContentsGeneral introductionJupiter and Io plasma torus (Target)Spectral diagnosis using EUV emissions (Approach)
Analysis of the data obtained by CASSINI/UVIS during its Jupiter flybyThe principle and method of the spectral diagnosisThe evaluation of the plasma parameters around the Io torusHot electron ratioAnother parameters
Development of the EUV spectroscope on board the earth-orbiting satelliteInstrumental overviewEntrance mirrorGratingDetectorMicrochannel plate with photocathodeResistive anode encoderThe shield structure and noise evaluationThe feasibility study of the observation for the Io torus
Summary
Future works24201211
MCP> 1 %RAE0.3 nm FWHMRAE10 30 < 1 cps/cm2
252526
F0.5mm
1RJ~10200mm, 5F27
Pt, Si, SiC
Pt, Si, SiC28SiCSiPt28
2929
3030Pt02% @30.4 nm22% @58.4 nm15% @83.4 nmSi---% @30.4 nm02% @58.4 nm15% @83.4 nmSiC00% @30.4 nm13% @58.4 nm30% @83.4 nmSiC30%
31CVD-SiCChemical Vapor Deposition (SiO2, H2, CH4SiCSiC
0.5 nmCVD-SiC
32
0.532CVD-SiC30 ~ 50%0.4 nmSample No. 10.34 nmNo. 30.36 nmNo. 1A0.42 nmNo. 2A0.32 nmNo. 5A0.39 nmNo. 6A0.30 nmNo. 7A0.22 nm
3333 1-CVD-SiC1800 Lines/mm22 nm
-Detector: MCPBias angle : 20 degreePhotocathode: CsI
2 mm Aluminum and 8 mm SUS304 shield1000 ~ 1200 km34
34CVD-SiC
0.5mm10, 2FWHMCVD-SiC
68,15, 20, 22, 26, 39 nmCVD-SiC
22nm
0.1nm
2nm39 1-CVD-SiC1800 Lines/mm22 nm
-Detector: MCPBias angle : 20 degreePhotocathode: CsI
2 mm Aluminum and 8 mm SUS304 shield1000 ~ 1200 kmMCP (Micro channel plate)MCP10um2
404040
201.510241414142
30-84 nm105-135 nmCsI / Bare1.5 - 25 - 100KBr/ Bare0.6 - 25 -80MCPRAEEUV2EUVMCP107RAE
SELENE/UPI/TEX3MCP ~0.1 pC7 bits128128 pixels
RAE : 1~100 k Ohm
43MCP + RAE (PHEBUS/BBM)MCP + RAE43MCPRAEEUV~10bits~RAE (Resistive Anode Encoder)+RuO2121
Q VADCADCAnalog to digital converter 14 bitsFPGA1-D RAE (~1 pC, 107 ele.)L1L2Q1Q2Q = Q1 + Q2
(x,y)
44LL44
2RAE MCP~~454546RAE10 bits (1024 * 1024 pixels)SELENE/UPI/TEX7 bits
(Point)RAEMCP, 10 pF1110 bits
RAE1
464647RAE 11mm (minimum)
RuO2RAE500 k100 k 50 k 10 k 5 k 1 k 10 pF18.13.611.790.420.180.043 pF6.931.380.700.100.070.02
[s]10pFAmptek/A2252.4 us10 k Ohm
474748RAE 2 -100 OhmRAEA225F
RAE10 k Ohm0.5 us200 300 OhmRAE1mm, 50 k Ohm484880um1A,10
20.08 mm0.3 1-CVD-SiC1800 Lines/mm22 nm
-Detector: MCPBias angle : 20 degreePhotocathode: CsI
2 mm Aluminum and 8 mm SUS304 shield1000 ~ 1200 km50
1 MeVAE8MAX model
1 MeV 1-CVD-SiC1800 Lines/mm22 nm
-Detector: MCPBias angle : 20 degreePhotocathode: CsI
2 mm Aluminum and 8 mm SUS304 shield1000 ~ 1200 km51
CASSINI/UVIS5003
CASSINI/UVISCASSINI/UVIS/EUV52CASSINI/UVISThe feasibility study of our future observation from the Earth-orbiting satellite130
53Ly-CASSINI/UVISThe feasibility study of our future observation from the Earth-orbiting satellite: 1 [eV] 1 % 500 [cm-3]54 VS VS VS
54Summary
CASSINI/UVIS1keV
3
155