SPICA現状報告
1. ESA-JAXA共同技術検討(CDF Study)とその後の技術検討
・検討結果が確定し公開された。 ・その後、サイエンス検討を重ねた結果、検討のベースラインを 望遠鏡口径2.5m、温度8K以下に冷却する「横置き」(Planck型)構造を ベースラインとすることとした。 (8-11ページ参照) ・以下のチームが核となり、ESAの技術検討結果および従来のSPICAの 成果などを用いて、衛星全体の設計、冷却系・望遠鏡設計を進めている。 来月には一次的な検討結果が得られる予定。 2.SPICA CV M5 対応チーム設置(6/4所長決定) ・宇宙研(JAXA)のΔMDR、SRRのための作業、および、ESAのCosmic Vision次回Mクラス公募への提案の作業を行うチームを組織し、設置した。 ・宇宙研赤外、国内赤外線天文学研究者、宇宙研宇宙物理学研究系、 宇宙研工学、研究開発本部、SE/PO室、国際調整担当の合同チーム チーム長:芝井、チーム長代理:小川博之、中川貴雄 ・プリプロジェクト再設置時までのチーム ・SPICAステアリンググループ(所内外)とSPICAタスクフォース(所内)が チームの活動をウォッチ。 光赤天連スペース将来計画シンポジウム 2015-07-08 13. SPICAチームの活動
3/25-27 SPICA(SAFARI?)コンソーシアム会議(Utrecht) ・ M5提案に向けて最終決断。 ・ SAFARIチームが欧州+カナダ+米国(一部研究者)に拡大 ・ 高分散中間赤外線分光機能、および系外惑星大気分光機能を 搭載する方向で検討を進める。 (3、4ページ参照) 3/31 SPICA全体会 5/18 学術会議天文宇宙分科会にて状況報告 この間、サイエンス検討・深化を進めた。(5-7ページ参照) 6/3-5 米国遠赤外コミュニティーワークショップにて講演 6/19 SPICA 科学レビュー(宇宙研)7/15 SPICA Science Case International Preview (Paris、宇宙研主催)
(13ぺージ参照)
7/31 SPICA全体会
9月 SPICAコンソーシアム会議(Bordeaux、SAFARI主催)
(12ぺージ参照)
1. SPICA mission overview
SPICA
– Space Infrared Telescope for Cosmology and Astrophysics3
SPICA is a space mission optimized for mid- and far-IR astronomy.
SPICA unveils the “dusty era” in the Universe (evolution of galaxies), and finds a route to habitable planets (formation of planetary systems).
SPICA is launched at ambient temperature, and cooled down in space.
(The cryo-cooler system is a key heritage of JAXA from IRTS and AKARI.) Japanese SMI is a mid-IR spectrometer covering 17-37 mm.
European SAFARI is a far-IR spectrometer covering 34-230 mm.
SPICA is a joint mission of JAXA and ESA with other international partners. SPICA is now in its re-definition phase in JAXA, and will go to the open
competition as an M-class mission of the ESA Cosmic Vision program.
Baseline specifications
Telescope : 2.5 m aperture, cooled below 8 K Core wavelength : 17–230 mm
(+ High-resolution spectrometer at 12–18 mm, Exoplanet instrument at 5–20 mm)
Orbit : S-E L2 Halo Orbit Launcher : JAXA H-3 Vehicle Launch Year : 2027-2028
H H
H H OD H
20 30 40 Si O O O Mg O HRS 12 14 16 18 λ (μm) 17.2 17.3 20 40 60 λ (μm)AKARI Mid-IR all-sky map
SPICA studies
how stars have been formed in galaxies along the history of the
Universe (Goal1: evolution of galaxies),
and
how planets have been formed in a disk around a forming star and
evolved to be habitable (Goal2: formation of planetary systems).
Enrichment of the Universe with metal and dust
leading to the formation of habitable worlds
4
IR spectroscopy
1. Dust bands (organic matter, mineral, ice)
2. Extinction-free metal lines
3. Molecular hydrogen lines
銀河成長と惑星系形成:
多様で豊かな宇宙を生んだ二大過程の解明
大目標
目的1. 銀河成長・物質進化過程の解明
- ダストに隠された銀河成長最盛期
(宇宙論的分光サーベイ、10平方度)
- 星生成と物質進化の相互作用(近傍銀河、4000個)
目的2.惑星系形成過程の解明
- ガスの精密定量による惑星形成シナリオの検証
- 惑星形成における水と氷の役割
- 惑星系外縁天体の起源
1. SPICA mission overview
Space infrared astronomy: from IRTS, AKARI to SPICA
6 IR lumino sit y densi ty ( L / Mpc 3 ) Goto+ 2010,A&A 514, 6 redshift IR galaxy Luminous IR Ultra-luminous IR
AKARI (Japan, Korea, Europe) 2006 ~2011 Spitzer (US) 2003 ~ IRTS (Japan) 1995
Herschel (Europe, US) 2009〜2013
Photometry
Exploration
Physics
Spectroscopy
SPICA
AKARI
IRTS
survey
mid-IR
spectroscopy
far-IR
spectroscopy
Evolution of galaxiesz=3
MIR Instrument (SMI)
Telescope
(NAOJ)
SPICA Data Center Launcher Science Community JP, Europe, US, KR, TW,,, Bus Module Payload Module Cryocooler
Focal Plane Instrument Assembly FIR Spectrometer (SAFARI) Exoplanet Spectroscopy (SPEChO) European countries NL + European countries + Canada & US
Focal Plane Attitude Sensor
1. SPICA mission overview
Work-sharing plan
Mirror M1 2.5 mf Mirror M2 Telescope Baffle PLM Metering Structure M2 Support Structure Telescope Optical Bench V-Groove thermal shields Supporting Bipod Telescope Shield (20 K) SVM Top Panel AOC StarTracker Cryo Warm Electronics
1K-JT Compressors 2ST Compressors 1K-JT Compressors
Planck-type PLM with a 2.5-m, <8K telescope
Current baseline configuration
ESA Stations Mission Operation Center (MOC) Science Operation Center (SOC) Science Data Center (SDC) JAXA Stations JAXA ESA Instrument Control Centers (ICCs)
ESA Science Center (ESC) Non-European User Community (Japan) (East Asia)
European Data Archive Center (ESDC) TBD
European User Community
Operational Ground Segment Science Ground Segment
9
運用体制(案)
JAXA宇宙科学研究所
国立天文台
ESA
プロジェクト推進体制 - SPICA コンソーシアム
SPICA
Consortium
SPICA-J Project SRON日本
ESA SMI Consortium SPEChO Consortium SAFARI Consortium NAOJ M5 Proposal Scientists (outside the instrument teams) 10 中間赤外観測 装置(日本) 名大、東大他 系外惑星大気分 光装置(検討中) 遠赤外線観測 装置(欧州+) 装置チーム外 研究者欧州
JAXA(参考)国際評価委員会
目的
SPICA計画について、科学的観点からの評価を得る。
日時・場所
2015年7月15日 Paris
評価委員
Michael Rowan-Robinson (UK),
Martin Bureau (UK), Anthony Jones (FR)
Peter Barthel (NL) Anthony Peter Jones (FR) Martin Harwit (US), George Helou (US)
Kazuhisa Mitsuda (JP),
ISAS
Saku Tsuneta, Masaki Fujimoto, Munetaka Ueno, Ikko FunakiSPICA
Hiroshi Shibai (PI), Takashi Onaka (PS),Hidehiro Kaneda (PI補佐), Kotaro Kohno (PS補佐) Daisuke Ishihara, Takehiko Wada, Naoki Isobe, Peter Roelfsema (NL), Bruce Sibthorpe (NL)
1. SPICA mission overview
Space infrared astronomy: from IRTS, AKARI to SPICA
12
10 – 50 AU
Case study
SPICA
AKARI
IRTS
survey
AKARI (Japan, Korea, Europe) 2006 ~2011 Spitzer (US) 2003 ~ IRTS (Japan) 1995
Herschel (Europe, US) 2009〜2013
SPICA
AKARI
IRTS
survey
mid-IR
spectroscopy
far-IR
spectroscopy
Universality
~1 AU
Planet-forming disk1. SPICA mission overview
Project schedule
13
Reviews & Phases
MDR SRR SDR Project Appr. Rev.pre-PDR Sys-PDR pre-CDR Sys-CDR PSR Launch
Phase-A PRR Phase-B1 SRR Phase-B2 PDR Phase-C CDR Phase-D QR? AR margin Phase-E1 Model & Tests
AI L Launch Operation PLM Caption FM SIA CQM (FPI) EM/STM Front Loading Q2 Q3 Q4 Q1 Q2 Q3 2025 2027 Q4 Q1 Q4 Q1 Q2 Q3 Q4Q1 Q2 Q2 Q4 Q2 Q3 Q4 Q1 Q2 Q3 Q4Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 CY 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024 2026 Q3 Q3 Q4 Q1 Q2 Q4 Q1 Q3 Q1 Q2 Q3 Q4 Q1 Q2 Q3 2028 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Phase-E JAXA ESA Phase-A System IVT ESA AIVT JAXA SVM AIVT PLM Comp Dev. SAFARI Consortium + SMI Consortium AIVT AIVT MCS Comp. Dev.
FPIA Design AIVT
FAS Design
Manufacture
FPIA IVT AIVT
PLM/CRYO Design manufacture
MCS Design / Manufacture MCS
SVM Design manufacture
FPIA FAS
STA Design / Manufacture
AIV IV STA Manufacture AIVT Manufacture SAFARI Design Manufacture
SAFARI Components Devekopment
AIVT
SMI Design manufacture
SMI Components Development
Phase-D Phase-C Phase-B AIVT AIVT SAFARI Manufacture AIVT manufacture SIA IVT AIVT SMI AIVT AIVT System IVT PLM IVT PLM/CRYO AIVT
FPI Warm Elechtronics
IOB-STM PLM/CRYO-STM MCS-EM SMI-CQM Detector Modules SAFARI-CQM Design
SPICA
10
5reduction !
K
SPICA
(8K)
1. SPICA mission overview
Importance of a cryogenically-cooled IR telescope
AKARI FIS-FTS JWST/MIRI Li mi ting Li ne F lux (5 -1h r) / Wm -2 10-16 10-18 10-17 10-19 100 1000 20 200 350 Wavelength / mm
2010's
1. SPICA mission overview
Dramatic improvement in the sensitivity
15 100 Improvement AKARI IRC
SPICA
2020's
ALMA 10-20 10 10-15 SPICA/SAFARI R=25000 R=300 SOFIA HERSCHEL Spitzer R=30001. SPICA mission overview
SPICA’s uniqueness in extra-galactic astronomy
16
ALMA
Sensitivity (5, 1 hour) of ALMA, SPICA, JWST and TMT, plotted on spectra of typical star-forming galaxies at z = 3 with different dust extinction values (AV = 0.3, 3, 30 mag).
TMT
AV = 0.3 mag
JWST
SPICA
SPICA fills the spectral gap between ALMA and JWST.
SPICA provides unique spectral tools
to study physics in dust-obscured galaxies.
2.1. Overview
Science goals and objectives
17
Top-level goal
Enrichment of the Universe with metal and dust, leading to the formation of habitable worlds
[SG1]
Evolution of galaxies
[SG2]
Formation of planetary systems
[SO1]
Star formation of distant galaxies
[SO2]
AGN outflow
[SO3]
Star formation in nearby galaxies
[SO4]
Gas dissipation in PPDs
[SO5]
Debris disks to solar system
[SO6]
Exoplanet atmosphere
SCIENCE GOALS
3.3. SPICA mission overview
Baseline design
18
Planck-type PLM with a 2.5 m, 8 K telescope
Front view
Side view
telescope baffle instrumentoptical bench telescope thermal shield V-groove thermal shields primary mirror secondary mirror cryo-cooler system payload module service module
3.3. SPICA mission overview
Telescope
19
Optical design
The 2.5 mφ optical design is scaled from the 2.0 mφ CDF study.
Optical specifications
Telescope type : Ritchey–Chrétien Entrance Pupil Diameter : 2.5 m Field of View : 30 arcmin
Wave Front Error : <1.4 mm rms Diffraction limited at 20 mm
Temperature
Launch: Room temperature Operation: < 8 K
Fabrication
ESA is in charge of the procurement of the telescope.
Technical Heritage
3.3. Configuration and specifications
Mechanical cryo-coolers
Cooling performance & reliability have improved based on AKARI & SMILES (e.g., flexure
bearings to support the piston and displacer, inner outgas control, microphonics control).
Design lifetime of 1K-JT has improved based on ASTRO-H 4K-JT with enhanced
contamination control. These technologies are reflected in the 2ST and 4K-JT coolers.
20K-class two-stage Stirling cooler (2ST) 4K-class J-T cooler (4K-JT) 1K-class J-T cooler (1K-JT) Cooling
objectives JT precooling STA + FPIA
FPIA (SAFARI+SMI) Cooling power (EOL) 200 mW@20 K, 1000 mW@100 K 40 [email protected] K 10 [email protected] K Input power < 90 W < 90 W < 75 W Lifetime > 3 years (goal: 5 years) >3 years (goal: 5 years) >3 years (goal: 5 years) Heritage AKARI (2006), JEM/SMILES (2009) ASTRO-H (2015) JEM/SMILES (2009) ASTRO-H (2015) Based on 4 K-JT
R&D status TRL6 (ASTRO-H) TRL6 (ASTRO-H) TRL5
Mechanical cryo-coolers in the baseline design have been developed in Japan.
3.3. Configuration and specifications
Focal-plane instruments
Spectral Resolution SPICA/SMI SPICA/SAFARI R = 3000 R = 300 Line Sensitivity Wavelength (mm) Wavelength (mm)SPICA Far-IR Instrument: SAFARI
SPICA Mid-IR Instrument: SMI
EChO instrument on SPICA: SPEChO
(LRS) 17-37 mm, Si:Sb, prism:10’ slit x 5 + 10’x10’ slit viewer, high mapping speed (MRS) 18-36 mm, Si:Sb, grating:1’ slit + beam-steering mirror, high sensitivity
(HRS) 12-18 mm, Si:As, grating: 6” slit + beam-steering mirror, high resolution 34-230 mm, TES, grating: 4 beams + beam-steering mirror, high sensitivity
5-20 mm, Si:As, grating, high-stability (10-3.5 in one eclipse) monitoring
R = 25000 R = 1000 JWST/MIRI-MRS Spitzer/IRS JWST/MIRI-LRS Spitzer/IRS 21
SAFARI
SMI
SMI
FAS
(Focal attitude sensor)
SPEChO
3.3. Configuration and specifications