the espresso detector system (stability) and first results of the...

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ESPRESSO, the E chelle SP ectrograph for R ocky E xoplanets and S table S pectroscopic O bservations is designed to measure the radial velocity down to 10 cm/s precision. It will be installed on ESO's VLT in order to achieve a gain of two magnitudes with respect to its predecessor HARPS, and permits to combine the light of up to four 8.2m telescopes. High precision Radial Velocity spectroscopy requires detector operation in an extremely stable mechanical and thermal environment; any tiny perturbation may affect the location of the detected spectral lines, affecting the instrument global performance. This paper describes the detector system stability considerations, from the detector selection, the CCD operating modes to the cryostat thermal/control design and the overall instrument system layout. Ways to design and measure the performance of the detectors and the detector system without the spectrograph are illustrated in particular with regard to simulation and lab testing. We will report test results obtained so far with the ultra-stable cryostat testbench. ABSTRACT O. Iwert, E. Ciattaglia, S. Deiries, H. Dekker, J. L. Lizon ESO, Karl-Schwarzschild-Str. 2, 85748 Garching, Germany THE ESPRESSO DETECTOR SYSTEM The SiC package has been stiffened considerably (Fig. 1 bottom), also allowing to interface the centre of the detector to cooling connections. The central thread will be used to mount a pin to allow symmetrical expansion around the centre. Cooling System with additional control loop ACKNOWLEDGMENTS E. Mueller developed the LabVIEW software for the ultrastable cryostat. Figure 8: (Left) Detector head inside the ultra-stable set-up (concept); (Right) Complete set-up photograph Each multi-spot projector consists of a pinhole mask producing an array of ~25000 spots on a 10 x 10 mm 2 field. Several projectors can be mounted close to the CCD surface across the field of one CCD. Measurement Results with a CCD mosaic of 2 x e2v CCD44-82 (HARPS-copy) inside the ultra-stable cryostat: Photo CCD 290. The ultra-stable cryostat enables optical centroiding stability tests of the detector system in the laboratory, independent of the actual spectrograph. It is comprised of an outer vacuum vessel, accommodating the actual detector head, various temperature sensors, an active sorption pump, several fibre-fed multispot- projectors with LED illumination, Lakeshore detector temperature controllers and a data logging/analysis system continuously calculating the centroids of projected spots. This facility will in the long term be used with the ESPRESSO detector cryostat (left section) and is currently used with a copy of the HARPS detector mosaic (2 x e2v CCD 44-82). Figure 3: (Left) Lab Test set-up with NGC DFE & PS; (Right) Warm first light images showing projection on 8 channels each (top and bottom). Two outputs of this very early sample are non-functional. The ESPRESSO Detector System (stability) and first results of the ultra-stable cryostat TEST FACILITY ULTRA-STABLE CRYOSTAT e2v CCD 290, 9k x 9k, 10 μm, 16 outputs in standard (blue) and high resistivity (red) version with improved Silicon Carbide (SiC) package and precise mounting. -0.5 0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 Expansion coefficient x 10^6 -200 -150 -100 -50 0 50 100 150 Temperature °C AleniaSiCdata AstriumSiCdata E2VTECHNOLOGIES At Room Temperature : Silicon: 2.3E-6 SiC: 2E-6 Invar : 1.3E-6 Kovar : 6.3E-6 Alumina : 8.2E-6 Aluminium nitride : 5.6E-6 Supplier 1 Supplier 2 Curve : TEC silicon Points :TEC Silicon Carbide -0.5 0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 Expansion coefficient x 10^6 -200 -150 -100 -50 0 50 100 150 Temperature °C AleniaSiCdata AstriumSiCdata E2VTECHNOLOGIES At Room Temperature : Silicon: 2.3E-6 SiC: 2E-6 Invar : 1.3E-6 Kovar : 6.3E-6 Alumina : 8.2E-6 Aluminium nitride : 5.6E-6 Supplier 1 Supplier 2 -0.5 0 0.5 1 1.5 2 2.5 3 3.5 4 4.5 Expansion coefficient x 10^6 -200 -150 -100 -50 0 50 100 150 Temperature °C AleniaSiCdata AstriumSiCdata E2VTECHNOLOGIES At Room Temperature : Silicon: 2.3E-6 SiC: 2E-6 Invar : 1.3E-6 Kovar : 6.3E-6 Alumina : 8.2E-6 Aluminium nitride : 5.6E-6 Supplier 1 Supplier 2 Curve : TEC silicon Points :TEC Silicon Carbide Instrument View Thermal Enclosures ESO CCD Controller NGC & CCD 290 early sample – warm first light Clock waveform measurement Special in-situ on CCD with NGC Clocking schemes Measurement set-up Fig. 4: Simulation of CCD package deformation - assuming worst case power consumption and 600 sec. integration time, slew time of 500 sec. Simulated Pixel Displacement during typical integration (worst case) Glass body 10x10x10 mm 3 Integrating Sphere Pinhole mask Fibre conn. 20 mm Detectors for red and blue arm Wipe Integrate Readout Power Consumption Detector Activity Conventional clocking scheme Envisaged ESPRESSO clocking scheme Figure 9: (Left) Multi-spot projector; (Right) Fibre set-up to feed four multi-spot projectors Figure 1: (Top) e2v CCD 290 mounted in ESO test set-up; (Bottom) SiC package backside view & Detail of stiffening ribs Figure 2: Thermal expansion coefficient of Silicon Carbide matched to Silicon Measuring the centroid positions in x,y,z of the generated spots on the CCDs and correlating the differential measurement graphs of individual temperature and pressure sensors inside the LabVIEW control program to centroid stability deviations, the sources for instabilities can be traced and studied (as shown below). At sufficient environmental (~ < 0.5 K) and CCD stability (~ < 40 mK) the centroids can be measured as a function of specific set-up parameters to systematically study their effects onto the centroid stability, e.g., F [spot intensity / location, CCD Temp., pixel history etc.] Figure 10: (Left) CCD mosaic and projector field; (Right) Resulting image and detail of spot pattern CCD controller FIERA LED controller PULPO CCD temperature controller Lakeshore 336 Lakeshore 218 LED drivers CCD cryostat Liquid nitrogen supply Pressure tubes and vacuum pump JUMOs TeePee High power LEDs Outer vacuum vessel Fig. 11: LabVIEW display (1) Early stage (2) More advanced (Top) Individual sensors, (Bottom) Centroid measurements, both over time 1 3 2 ∆T Fig. 12: (3) Optimized system set-up & optimized ambient conditions: (Top) Individual sensors in differential display; (Bottom) Centroid measurements x, y, z of both detectors < 5nm over time. Centroid nm ∆T & ∆ P Fig 7: (Left) Instrument Vacuum vessel with opto-mechanical bench and red and blue CCD cryostats on top. (Right) Thermal Enclosures 1T … 3T with different stabilization Fig 5: (Left) Parallel Clock Pulse shapes as a result of NGC and CCD; (Right) Envisaged ‘dummy’ clocking to result in more equalized power consumption Fig 6: (Left) CCD Cryostat (Right) Cut view of CCD Cryostat Three temperature control loops with increasing precision are used: (1) LN 2 flow +/- 1K (2) Larger thermal capacity with about +/- 0.1 K (3) CCD control loop Lakeshore +/- some mK (1) (2) (3) ∆ T ~ 70 mK Total ∆ ~ 2.64 nm ∆ X ~ 4.04 nm ∆ Y ~ 3.5 nm ∆ Z ~ 1.8 nm

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Page 1: The ESPRESSO Detector System (stability) and first results of the …ridl.cfd.rit.edu/products/publications/SDW/SDW 2013... · 2013-11-01 · with regard to simulation and lab testing

ESPRESSO, the Echelle SPectrograph for Rocky Exoplanets and Stable Spectroscopic Observations is designed to measure the radialvelocity down to 10 cm/s precision. It will be installed on ESO's VLT in order to achieve a gain of two magnitudes with respect to itspredecessor HARPS, and permits to combine the light of up to four 8.2m telescopes.High precision Radial Velocity spectroscopy requires detector operation in an extremely stable mechanical and thermal environment; any tinyperturbation may affect the location of the detected spectral lines, affecting the instrument global performance. This paper describes thedetector system stability considerations, from the detector selection, the CCD operating modes to the cryostat thermal/control design and theoverall instrument system layout.Ways to design and measure the performance of the detectors and the detector system without the spectrograph are illustrated in particularwith regard to simulation and lab testing. We will report test results obtained so far with the ultra-stable cryostat testbench.

ABSTRACT

O. Iwert, E. Ciattaglia, S. Deiries, H. Dekker, J. L. Lizon ESO, Karl-Schwarzschild-Str. 2, 85748 Garching, Germany

THE ESPRESSO DETECTOR SYSTEM

The SiC package has been stiffenedconsiderably (Fig. 1 bottom), also allowingto interface the centre of the detector tocooling connections. The central threadwill be used to mount a pin to allowsymmetrical expansion around the centre.

Cooling System with additional control loop

ACKNOWLEDGMENTSE. Mueller developed the LabVIEW software for the ultrastable cryostat.

Figure 8: (Left) Detector head insidethe ultra-stable set-up (concept);(Right) Complete set-up photograph

Each multi-spot projector consists of a pinhole mask producing an array of ~25000spots on a 10 x 10 mm2 field. Several projectors can be mounted close to the CCDsurface across the field of one CCD.

Measurement Results with a CCD mosaic of 2 x e2v CCD44-82 (HARPS-copy) inside the ultra-stable cryostat:

Photo CCD 290.

The ultra-stable cryostat enables optical centroiding stability tests of the detector systemin the laboratory, independent of the actual spectrograph.It is comprised of an outer vacuum vessel, accommodating the actual detector head,various temperature sensors, an active sorption pump, several fibre-fed multispot-projectors with LED illumination, Lakeshore detector temperature controllers and a datalogging/analysis system continuously calculating the centroids of projected spots. Thisfacility will in the long term be used with the ESPRESSO detector cryostat (left section)and is currently used with a copy of the HARPS detector mosaic (2 x e2v CCD 44-82).

Figure 3: (Left) Lab Test set-up with NGC DFE & PS;(Right) Warm first light images showing projection on 8 channels each (top and bottom). Two outputs of this very early sample are non-functional.

The ESPRESSO Detector System (stability)and first results of the ultra-stable cryostat

TEST FACILITY ULTRA-STABLE CRYOSTAT

e2v CCD 290, 9k x 9k, 10 µm, 16 outputs in standard (blue) and high resistivity (red) version with improved Silicon Carbide (SiC) package and precise mounting.

-0.5

0

0.5

1

1.5

2

2.5

3

3.5

4

4.5

Expa

nsion

coeff

icien

t x 10

^6

-200 -150 -100 -50 0 50 100 150 Temperature °CAlenia SiC data Astrium SiC data

E2V TECHNOLOGIES

At Room Temperature :Silicon : 2.3E-6SiC : 2E-6Invar : 1.3E-6Kovar : 6.3E-6Alumina : 8.2E-6Aluminium nitride : 5.6E-6

Supplier 1 Supplier 2

Curve : TEC siliconPoints :TEC Silicon Carbide

-0.5

0

0.5

1

1.5

2

2.5

3

3.5

4

4.5

Expa

nsion

coeff

icien

t x 10

^6

-200 -150 -100 -50 0 50 100 150 Temperature °CAlenia SiC data Astrium SiC data

E2V TECHNOLOGIES

At Room Temperature :Silicon : 2.3E-6SiC : 2E-6Invar : 1.3E-6Kovar : 6.3E-6Alumina : 8.2E-6Aluminium nitride : 5.6E-6

Supplier 1 Supplier 2

-0.5

0

0.5

1

1.5

2

2.5

3

3.5

4

4.5

Expa

nsion

coeff

icien

t x 10

^6

-200 -150 -100 -50 0 50 100 150 Temperature °CAlenia SiC data Astrium SiC data

E2V TECHNOLOGIES

At Room Temperature :Silicon : 2.3E-6SiC : 2E-6Invar : 1.3E-6Kovar : 6.3E-6Alumina : 8.2E-6Aluminium nitride : 5.6E-6

Supplier 1 Supplier 2

Curve : TEC siliconPoints :TEC Silicon Carbide

Instrument View Thermal Enclosures

ESO CCD Controller NGC & CCD 290 early sample – warm first light

Clock waveform measurement Special in-situ on CCD with NGC Clocking schemes

Measurement set-up

Fig. 4: Simulation of CCD package deformation - assuming worst case power consumption and 600 sec. integration time, slew time of 500 sec.

Simulated Pixel Displacement during typical integration (worst case)

Glass body10x10x10 mm3

Integrating

Sphere

Pinhole mask

Fibre conn.

20mm

Detectors for red and blue arm

Wipe Integrate Readout

Power

Consumption

Detector

Activity

Conventional clocking scheme

Envisaged ESPRESSO clocking scheme

Figure 9: (Left) Multi-spot projector;(Right) Fibre set-up to feed four multi-spot projectors

Figure 1: (Top) e2v CCD 290 mounted in ESO test set-up; (Bottom) SiC package backside view & Detail of stiffening ribs

Figure 2: Thermal expansion coefficientof Silicon Carbide matched to Silicon

Measuring the centroid positions in x,y,z of the generated spots on the CCDs andcorrelating the differential measurement graphs of individual temperature and pressuresensors inside the LabVIEW control program to centroid stability deviations, the sourcesfor instabilities can be traced and studied (as shown below).At sufficient environmental (~ < 0.5 K) and CCD stability (~ < 40 mK) the centroids canbe measured as a function of specific set-up parameters to systematically study theireffects onto the centroid stability, e.g., F [spot intensity / location, CCD Temp., pixelhistory etc.]

Figure 10: (Left) CCD mosaic and projector field;(Right) Resulting image and detail of spotpattern

CCD controller

FIERA

LED controller PULPO

CCD temperature controller Lakeshore 336

Lakeshore 218

LED drivers

CCDcryostat

Liquid nitrogen supply

Pressure tubes and vacuum pump

JUMOsTeePee

High power LEDs

Outer vacuumvessel

Fig. 11:LabVIEW display(1) Early stage(2) More advanced(Top) Individual sensors,(Bottom) Centroidmeasurements, both over time

1

3

2 ∆T

Fig. 12:(3) Optimized system set-up & optimized ambient conditions:

(Top) Individual sensors in differential display;

(Bottom) Centroidmeasurementsx, y, z of both detectors < 5nm over time.

Centroid nm

∆T & ∆ P

Fig 7: (Left) Instrument Vacuum vessel with opto-mechanical bench and red and blueCCD cryostats on top. (Right) Thermal Enclosures 1T … 3T with different stabilization

Fig 5: (Left) Parallel Clock Pulse shapes as a result of NGC and CCD;(Right) Envisaged ‘dummy’ clocking to result in more equalized power consumption

Fig 6: (Left) CCD Cryostat (Right) Cut view of CCD Cryostat

Three temperature control loops with increasing precision are used:(1) LN 2 flow +/- 1K(2) Larger thermal capacity with about +/- 0.1 K(3) CCD control loop Lakeshore +/- some mK

(1) (2) (3)

∆ T ~ 70 mK

Total ∆ ~ 2.64 nm ∆ X ~ 4.04 nm ∆ Y ~ 3.5 nm ∆ Z ~ 1.8 nm