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SPHERE(Spectro-Polarimetric High-contrast Exoplanet REsearch)
A Planet Finder Instrument for the VLTJeanJean--Luc Beuzit (PI), Markus Feldt (CoLuc Beuzit (PI), Markus Feldt (Co--PI),PI),
David Mouillet (PS), Pascal Puget (PM), Kjetil Dohlen (SE)David Mouillet (PS), Pascal Puget (PM), Kjetil Dohlen (SE)F. Wildi (AIT), T. Fusco, C. Petit (AO)F. Wildi (AIT), T. Fusco, C. Petit (AO)
and numerous participants from 12 European institutes !and numerous participants from 12 European institutes !
LAOG, MPIA, LAM, ONERA, LESIA, INAF, Geneva Observatory,LAOG, MPIA, LAM, ONERA, LESIA, INAF, Geneva Observatory,LUAN, ASTRON, ETHLUAN, ASTRON, ETH--Z, UvA, ESOZ, UvA, ESO
CoCo--IsIs: D. Mouillet (LAOG, Grenoble), T. Henning (MPIA, Heidelberg),: D. Mouillet (LAOG, Grenoble), T. Henning (MPIA, Heidelberg),C. Moutou (LAM, Marseille), A. Boccaletti (LESIA, Paris), S. UdryC. Moutou (LAM, Marseille), A. Boccaletti (LESIA, Paris), S. Udry
(Observatoire de Genève), M. Turrato (INAF, Padova), H.M. Schmid(Observatoire de Genève), M. Turrato (INAF, Padova), H.M. Schmid(ETH, Zurich), F. Vakili (LUAN, Nice), R. Waters (UvA, Amsterdam)(ETH, Zurich), F. Vakili (LUAN, Nice), R. Waters (UvA, Amsterdam)
Science objectivesHigh contrast imaging down to planetary massesInvestigate large target sample: statistics, variety ofstellar classes, evolutionary trendsComplete the accessible period windowFirst order characterization of the atmosphere (clouds,dust content, Methane, water absorption, effectivetemperature, radius, dust polarization)Understand the planetary system origins
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Science objectives
Radial Velocity
Large Surveys
HC & HAR Imaging
Lensing
Transits
StarsStars -- BDsBDs
BDsBDs -- PlanetsPlanets
High contrast detection capabilityHigh contrast detection capabilityExtreme AO (turbulence correction)Extreme AO (turbulence correction)
feed coronagraph with well corrected WFfeed coronagraph with well corrected WFSR ~ 90% in HSR ~ 90% in H--bandband
Coronagraphy (removal of diffraction pattern)Coronagraphy (removal of diffraction pattern)high dynamics at short separationshigh dynamics at short separations
Differential detection (removal of residual defects)Differential detection (removal of residual defects)calibration of non common path aberrationscalibration of non common path aberrationspupil and field stabilitypupil and field stabilitysmart post processing toolssmart post processing tools
High sensitivityHigh sensitivityoptimal correction up to V ~ 9optimal correction up to V ~ 9--1010
High level requirementsScientific requirementsScientific requirements
Gain up to 2 orders of magnitude in contrast as comparedGain up to 2 orders of magnitude in contrast as comparedto current instrumentationto current instrumentation
Reach short separations: 0.1’’Reach short separations: 0.1’’ –– 3” (13” (1-- 100AU)100AU)Survey a large number of targetsSurvey a large number of targets
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Common Path
Foreoptics
ExtremeAO
NIRCoronagraph
VisCoronagraph
ZIMPOL
IFS
IRDIS
High frequency AO correction (41x41 act.)High stability : image / pupil controlVisible – NIR Refraction correctionFoV = 12.5’’40x40 SH-WFS in visible1.2 KHz, RON < 1e-
Pupil apodisation,Focal masks: Lyot, A4Q, ALC.IR-TT sensor for fine entering
Coronagraphic imaging:Dual polarimetry, direct BB + NB.
= 0.5 – 0.9 µm,/2D @ 0.6 µm, FoV = 3.5”
0.95 – 1.35/1.65 µm/2D @ 0.95 µm,
Spectral resolution:R = 54 / 33FoV = 1.77”
0.95 – 2.32 µm; /2D @ 0.95 µmDifferential imaging: 2 wavelengths,R~30, FoV = 12.5’’Long Slit spectro: R~50 & 400Differential polarizationNasmyth platform, static bench,
Temperature control, cleanliness controlActive vibration control
Beam control(DM, TT, PTT,derotation)Pola controlCalibration
Concept overview
(i) modes and operations(i) modes and operations
11 ‘’ x 12.5’’
Astrometric accuracy: 0.5 – 2 mas(depending on SNR)
> 1.77 ‘’ (3’’)
10-6 (10-7) at 0.5”
5. 10-6 (5. 10-7) at 0.5”
Simultaneous use ofY-J band with IFSDual imaging in H
Multiplex advantage forfield and spectral rangeMutual support: falsealarm reduction, operation,calibrationImmediate companionearly classification
Combined useand advantagesof IRDIS/DBI
and IFS
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ImplementationImplementationCPICPI
IRDISIRDIS IFSIFS
ZIMPOLZIMPOL
ITTMITTM
PTTMPTTM
DMDM
DTTPDTTP
DTTSDTTS
WFSWFS
DeDe--rotatorrotator
VIS ADCVIS ADCNIR ADCNIR ADC
Focus 1Focus 1
Focus 2Focus 2
Focus 3Focus 3
Focus 4Focus 4
NIR coronoNIR corono
VIS coronoVIS corono
HWP2HWP2
HWP1HWP1
Polar CalPolar Cal
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NIR ADCNIR ADC
VIS ADCVIS ADC
WFSWFSDTTPDTTP
Focus 2Focus 2
FiltersFiltersSpatial filterSpatial filter
NIRNIRVISVIS
ZIMPOLZIMPOL
VISVIS
WFSWFS
IRDIFSIRDIFS
DTTSDTTSApodizerApodizer
AO systemCorrect for turbulence
provide a corrected area of 1.5-2 arcsec diameter60 nm rms on corrected modes => (90% SR in H for typical Paranal
conditions)Residual jitter smaller than ±3 (goal 1.5) mas rmsOptimal perf for V-mag GS < 9 (goal 10)Good correction (better than NAOS) for GS mag < 12 (goal 15)
To ensure system stabilityTo ensure system stabilityOptical axis wrt to coronagraphic deviceOptical axis wrt to coronagraphic device < 0.5 mas< 0.5 mas (goal 0.2)(goal 0.2)Beam shift on optical surfacesBeam shift on optical surfaces < 0.2% (goal 0.1) of the full pupil< 0.2% (goal 0.1) of the full pupil
diameterdiameterNon common path aberrations (down to coronagraph device)Non common path aberrations (down to coronagraph device) < 15 nm rms< 15 nm rms
To provide useful data for image postTo provide useful data for image post--processingprocessingStorage of WFS and control dataStorage of WFS and control dataEstimation of turbulence and system critical parametersEstimation of turbulence and system critical parametersMeasurement of IRDIS internal defects (differential aberrations)Measurement of IRDIS internal defects (differential aberrations)
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AO System
SPARTA: Standard Platformfor Adaptive optics RealTime Applications
SPHERE Deformable Mirror
CILAS piezoCILAS piezo--stack DMstack DMdelivered end 2007delivered end 2007Surface quality: 5nm rmsSurface quality: 5nm rms
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Fast Image Tip-tilt
“X” bandwidth is 700 Hz at“X” bandwidth is 700 Hz at --3dB3dBphase shift ofphase shift of --1515°° at 80Hzat 80Hz“Y” bandwidth is 891 Hz at“Y” bandwidth is 891 Hz at --3dB3dBphase shift ofphase shift of --1010°° at 80 Hzat 80 HzGoal 1000HzGoal 1000Hz
Freq Resp 2:1 CBFX.DAT
180deg
-20
Phase
kHz10.0110 Hz (Log)
Freq Resp 2:1 CBFY.DAT
Freq Resp 2:1 CBFY.DAT3
dB
-27
Mag (dB)
kHz10.0110 Hz (Log)
Freq Resp 2:1 CBFX.DAT
X:80.84093 Hz Y:165.1293 deg
X:80.84093 Hz Y:170.242 deg
X:891.8301 Hz Y:-3.277 dB
X:700.2723 Hz Y:-2.966 dB
prototypeprototype
1.2 kHz, CCD220-based wavefront sensorBenefits from the Opticon JRA1 reasearch program (EU funded)Benefits from the Opticon JRA1 reasearch program (EU funded)Common with the VLT AOCommon with the VLT AO--facilityfacility1. pixels, square 24 m2. 100% fill factor and 240x240 square grid array of pixels.3. low read noise of < 1 e-/pixel and goal of 0.1 e-/pixel.4. range of operating frame rates from 25 frames/s (fps) to 1200fps
NGC development (ESO)NGC development (ESO)Spatially Filtered SHSpatially Filtered SH
Optimization of theOptimization of thespatial filter sizespatial filter sizeStudy of BB impactStudy of BB impactWCOG : confirmation ofWCOG : confirmation ofthe gain in perfthe gain in perf(simulation &(simulation &experimentation)experimentation)
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Main components – RTCBased on SPARTA platformBased on SPARTA platform
Consortium specifications (+ algo)Consortium specifications (+ algo)ESO developmentESO development
Main featuresMain featuresvery small global delay (~ 1ms)very small global delay (~ 1ms)
+ large number of actuators+ large number of actuatorshybrid control lawhybrid control law
LQG (Kalman filter based) for TTLQG (Kalman filter based) for TTOMGI for higher modesOMGI for higher modes
additional features to deal with SAXO specificities (DTTS, PTTS)additional features to deal with SAXO specificities (DTTS, PTTS)
StatusStatusSpecifications OKSpecifications OKDevelopment:Development:
Various version (drops) available for SPHERE during SPARTA developmentVarious version (drops) available for SPHERE during SPARTA development=> optimization of the AIT period => reduction of risks and planning drifts.=> optimization of the AIT period => reduction of risks and planning drifts.First version to be delivered midFirst version to be delivered mid--July 2009July 2009
Main components – Aux. sensorsDifferential TipDifferential Tip--Tilt SensorTilt Sensor
IR camera located just beforeIR camera located just beforethe coronagraph maskthe coronagraph mask1 to 10 % of the IR flux for this sensor1 to 10 % of the IR flux for this sensorWCoG measurementWCoG measurementcontrol of a diff. tip tilt platecontrol of a diff. tip tilt plateclosed loop schemeclosed loop scheme –– 11--10 Hz10 Hzadditional capability: focus check between twoadditional capability: focus check between twoobservationsobservationsCould potentially be used to implement onCould potentially be used to implement on--line phaseline phasediversitydiversity
Pupil TipPupil Tip--Tilt SensorTilt SensorUse of SH data (subUse of SH data (sub--aperture. intensities)aperture. intensities)PTTM close to the entrance focal planePTTM close to the entrance focal planeClosed loop schemeClosed loop schemeFrame rate ~ 0.1 HzFrame rate ~ 0.1 HzResidual beam shift < 0.2 % of the full pupil diameterResidual beam shift < 0.2 % of the full pupil diameter
DTTSDTTSVisVis
WFSWFSRTCRTC
DM & TTMDM & TTM
DTTPDTTP
VIS/IRVIS/IR 1/99 %1/99 %
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CoronagraphsClassical Lyot coronagraph
Proven concept, existing on sky, no substrateLimited to external regions (> 0.5’’)
4Q phase mask Y, J, HWell studied, existing in NACO for narrow bandAllow to explore inner regions (down to /D)On-going R&D
Apodized pupil LyotOptimized for Y, J, H
Other concepts (modular design)New ideas like ZOG, Annular Grove Phase Mask, etc.
IRDIS, IFS and ZIMPOL have pupil imaging lenses
SPHERE A4Q focal plane mask prototype
18 µm diameter tungsten wires
Airy diameter in H band
18 µm diameter tungsten wires
Airy diameter in H band
close-up showing the tungstenwires placed to mask theedges of the wave plates
the complete assembled device
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A4Q Prototype
1,E-07
1,E-06
1,E-05
1,E-04
1,E-03
1,E-02
1,E-01
1,E+000 2 4 6 8 10 12 14
separation in lambda/D
PSF - YPSF - JPSF - H4QPM - Y4QPM - J4QPM - H
1,E-07
1,E-06
1,E-05
1,E-04
1,E-03
1,E-02
1,E-01
1,E+000 2 4 6 8 10 12 14
separation in lambda/D
PSF - H1PSF - H24QPM - H14QPM - H24QPM - H1-H2
H1
H2
H1-H2
Raw performance
Dual-bandperformance
ImplementationImplementationCPICPI
IRDISIRDIS IFSIFS
ZIMPOLZIMPOL
ITTMITTM
PTTMPTTM
DMDM
DTTPDTTP
DTTSDTTS
WFSWFS
DeDe--rotatorrotator
VIS ADCVIS ADCNIR ADCNIR ADC
Focus 1Focus 1
Focus 2Focus 2
Focus 3Focus 3
Focus 4Focus 4
NIR coronoNIR corono
VIS coronoVIS corono
HWP2HWP2
HWP1HWP1
Polar CalPolar Cal
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IRDIS dual beam imager
Old M0 star, 10 pc
10 MJ planet at 0.1"1 MJ planet at 0.2"
Young M0 star, 40 pc
ImplementationImplementationCPICPI
IRDISIRDIS IFSIFS
ZIMPOLZIMPOL
ITTMITTM
PTTMPTTM
DMDM
DTTPDTTP
DTTSDTTS
WFSWFS
DeDe--rotatorrotator
VIS ADCVIS ADCNIR ADCNIR ADC
Focus 1Focus 1
Focus 2Focus 2
Focus 3Focus 3
Focus 4Focus 4
NIR coronoNIR corono
VIS coronoVIS corono
HWP2HWP2
HWP1HWP1
Polar CalPolar Cal
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ZIMPOL performance
ImplementationImplementationCPICPI
IRDISIRDIS IFSIFS
ZIMPOLZIMPOL
ITTMITTM
PTTMPTTM
DMDM
DTTPDTTP
DTTSDTTS
WFSWFS
DeDe--rotatorrotator
VIS ADCVIS ADCNIR ADCNIR ADC
Focus 1Focus 1
Focus 2Focus 2
Focus 3Focus 3
Focus 4Focus 4
NIR coronoNIR corono
VIS coronoVIS corono
HWP2HWP2
HWP1HWP1
Polar CalPolar Cal
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Journées FOST/GRIL ExoJournées FOST/GRIL Exo--planètes 19planètes 19--20 D20 D
Principe et ordres de grandeursPrincipe et ordres de grandeursPerformance en forte évolutionPerformance en forte évolution
101066
101088
2000’s2000’s
2010’s2010’s
2020’s2020’s
~ all stars~ all stars
R <~ 12R <~ 12
R <~ 9R <~ 9
R <~ ?R <~ ?
ConclusionsVery challenging project !Now at manufacturing stageAt Paranal in early 2011Main science outputs by ~2015 for both:
Large surveys for statistical approaches, broad targetselectionIn-depth characterization of specific systems
Critical step before further exoplanet studies in theELT era for
Technological developmentSystem/calibration/operational experienceScientific preparation on the given available target sample
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Thank you !
NNactact-- FFsampsamp-- : the necessary trade: the necessary trade--offsoffs
•• NNactact
•• FFsampsamp
•• (WFS(WFS--im)im)
Corrected areaCorrected area NNactact
ContrastContrast
(profil(profil (N(Nactact))--8/3)8/3)
ContrastContrast (F(Fsampsamp))22
Noise effectsNoise effects --22
WFS spectral bandwidthWFS spectral bandwidthVIS detectorVIS detector
Gain in limit magGain in limit magcontrastcontrast
WFS FluxWFS Flux (N(Nactact))Loss in limit magLoss in limit mag
WFS FluxWFS Flux (F(Fsampsamp))--11
Loss in limit magLoss in limit mag
Chromatism effectsChromatism effectscontrastcontrast
GAINS LOSSESGAINS LOSSES
Complex tradeComplex trade--offs:offs: depends on scientific requirements (ultimate contrast,depends on scientific requirements (ultimate contrast,number of targets) and atmospheric conditionsnumber of targets) and atmospheric conditions
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SAXO error budget41x41 actuators => corrected area +/41x41 actuators => corrected area +/-- 0.82” in H0.82” in H“Simplified” Error budget (nm rms) for SAXO“Simplified” Error budget (nm rms) for SAXO
Telescope/instrument defectsTelescope/instrument defectsin the corrected area : static / quasiin the corrected area : static / quasi--static => fully corrected by AOstatic => fully corrected by AOhigh freq : no correctionhigh freq : no correction -- included in the global system error budgetincluded in the global system error budget
Error sources Low frequencies (nm) High frequencies (nm)
Seeing 0.65 0.85 0.65 0.85
total for atmospheric limitations 11 14 9 11
total for DM errors 11 (7) 13 (9) 52 63
Total for temporal errors 19 (15) 23 (18) - -
Total for residual aliasing error 20 (13) 32 (23) - -
Total for noise related errors 42 (35) 44 (36) - -
Total for mis-calibration errors 10 (5) 10 (5)
TOTAL for the AO main AO loop 54 (43) 62 (49) 52.8 64.0
41x41 act.41x41 act.
1.2 KHz1.2 KHz
Filtered SHFiltered SH--WFSWFS
EMCCD, WCoG,EMCCD, WCoG,BB WFSBB WFSNCPA comp.NCPA comp.
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