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1 SOLAR-C 1
2 SOLAR-C A: B:
3 (1981 ) (1991 ) (2006 ) ( 1.1) X X X ( ) 1990 SoHO TRACE /ASTRO-A ( ) /SOLAR-A ( ) /USA/UK SOLAR-C /SOLAR-B (2006-) / US/ UK/ ESA(Norway) 1.1: 3
4 1.2: 2006 (SOLAR-B) (SOT)()(0.2 ) X (XRT)(EIS) (1 ) (0.2 ) ( 1.2) ( ) ( 3.2 ) 1990 SoHO ( 1.3) 4
5 1.3: 11 ( ) (CME) 1.2. SOLAR-C 2 5
6 A: ( ) B: ( ) SOLAR-C 1 2 SOLAR-C (1) (2) (3) (4) 6
7 2. A: 2.1. A: ( ) 2006 (EUV)( ) 1AU SOLAR-C 7
8 2.1 SOLAR-C A (1) (2) 1) 2) X ( ) TBD TBD 1AU (TBR) 45 (2.3.3 ) 2.2. A 1) 2) (1990 ) tachocline 0.7 8
9 2.1: ( ) tachocline ( ) ( 2.1 ) ( 2.1 ) SoHO 60 ( 2.1 ) 2.2: 9
10 ( 2.2) ( 1.3) X X X ( 2.3) (IPS) 10
11 2.3: X X X X ( ) 3 ( ) 1 11 (CME) (CME) CME Solar Energetic Particle(SEP) 11
12 AU (*) 60 (*) 1 AU km/s 45 V 23 km/s km/s 150 mn (1) JAXA (2) JAXA NAL mn (TBR) (1) 30 mn (2) 150 mn TBD 12
13 TBD TBD TBD TBD X ( ) ()
14 2.4 1 AU STEREO 1.2m 0.5 AU kbps
15 3. B: 3.1. B (SOLAR-B) (SOT) 50cm ()( nm ) 10 ( ) ( ) B: () SOLAR-C (UV) (EUV) 15
16 3.1 SOLAR-C B 1) ( 50cm ) ( ) 2) (0.5 ) (1 ) 3) (0.2 ) TBD TBD X (1 ) () (2 ) ( 10 ) 16
17 ( 3.2) 3.1: 3.2:
18 3.3: ( ) ( ) ( ) 3. ( ) CaIIH ( ) EIS 40 SoHO SUMER 15 ( ) SoHO SUMER SUMER ( 3.3) ,
19 3.4: 3.5: ( 3.4) ( ) ( 3.5) 3.3 ( 1) ( 3.3) 19
20 3.6: 3.7: XRT ( ) ( )( 3.3) 3.6 ( 1) 20
21 3.8: X 3.7 expansion factor ( 3.8) 1 X
22 cm cm ( ) 1200Å 8500Å 20cm (0.5 ) 100 Å 1000Å cm (0.5 ) 100 Å 300Å X XUV (XDT) 22
23 (4k 4k ) () 1000 ( ) ( ) 23
24 4. SOLAR-C ISAS/JAXA NASA PPARC STFC ESA SOLAR-C ISAS/JAXA SOLAR-C ( ) : ( ) : (JAXA ) ( ) 24
25 5. SOLAR-C WG 2008 A B SOLAR-C 5.1SOLAR-C SOLAR-C 2014 ( A) ESA 2015 Solar Orbiter ( 5.1) ( B) NASA Solar Dynamics Observatory (SDO) ( 5.1) SDO 25
26 CY HINODE SOLAR-C ATST(NSF) (1) B A SDO(NASA) (2) Solar Orbiter(ESA) (3) (1) ATST (Advanced Technology Solar Telescope) (NSF) 4m() 2014 (AO) 0.1 (2) SDO (Solar Dynamics Observatory) (NASA) SoHO SoHO (1 ) (3) Solar Orbiter (ESA) 0.21AU (0.05 ) : SOLAR-C 26
erg ( ) 2 ( ) 3 E mag = B2 B L 8π L G 10 5 erg (1) km 3.1
4 1 2 3 10 29 10 32 erg ( ) 2 ( ) 3 E mag = B2 B L 8π L3 4 10 32 100G 10 5 erg (1) km 3.1 3.1.1 100 t D t D L2 η 1014 sec ( ) 3/2 T η = 10 4 cm 2 /s 10 6 (2) K B t = η 2 B (3) ( L ) 2 ( 10 4 km η 10 4
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小惑星探査ミッション はやぶさ 2 第 回宇宙科学シンポジウム 年 月 日 宇宙航空研究開発機構宇宙科学研究所 吉川真 ( ) はやぶさ 2 プロジェクト準備チーム 1 現状のまとめ はやぶさ のカプセルが地球帰還し はやぶさ ミッションの経験がフルに生かせる状況になった 来年度 (H23 年度 ) に はやぶさ 2 の予算が認められた 今年度内のプロジェクト移行を目指して いろいろな作業を継続している
