Download - Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

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Page 1: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Camera CCD in sviluppo all’XUVLab per un esperimento su razzo, precursore dell’esperimento UVC del Solar Orbiter

Compact (72mm x 72mm x 50mm)

Lightweight Fully vacuum compatible 4096 x 4096 maximum

CCD format Three-stage Peltier cooler Two available thermal

links between the CCD and the TEC (ΔT=-85°C/-60°C)

Very low noise preamplifier stage (1.8 nV/Hz r.m.s.)

Page 2: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Forme d’onda del CCD (fasi orizzontali in alto e verticali in basso) come appaiono ad uno strumento chiamato “analizzatore di stati logici”

Page 3: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Problemi dei rivelatori UV

low UV sensitivity, unstable,

not radiation hard, highly visible sensitive

PhotomultipliersPhotomultipliers

CCDCCD

Photodiodes

(a-Si, treated Si, Al)

Photodiodes

(a-Si, treated Si, Al)

Micro-Channel PlatesMicro-Channel Plates high voltage, hygroscopic photocathodes, unstable gain, operated in UHV

low UV sensitivity, unstable,

not radiation hard, highly visible sensitive

high voltage, 110 nm,

low fluxes, dark current

Page 4: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Ideal UV detector for space

visible blindnessvery low noise

high sensitivity to XUV photonschemical stability

radiation hardness

Requests

Page 5: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Specifiche per i rivelatori del Solar Orbiter

• Solar blindness < 10-7

• Operating temperature ± 50°C• Frame rate 1000 s -1

• Frame format 2K 2K • Pixel size < 20 m• Radiation hardness 50 Krad• Weight 1 kg

Common specification requirements for the imaging and spectroscopic instruments for remote sensing are

Photon fluxes (counts/s/px)

Imaging 103

Spectroscopy 102-103

3-D spectroscopy 105

Photon fluxes (counts/s/px)

Imaging 103

Spectroscopy 102-103

3-D spectroscopy 105

Page 6: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Rivelatori UV disponibiliPhoton Counting

MCP + XDL

MCP + APS

MCP + CID

Advantages Photon counting Solar blindness Radiation hardness Spatialised Operating @ Tamb

Disadvantages Efficiency < 30% High voltage biases Weight Spatial resolution (centroid

required) External electronics (to be

shielded!)

Charge integration

None!

CCD is not rad-hard

Page 7: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Alternativa: nuovi materiali fotosensibili

Eg = 5.5 eV dark current < 1 pA

visible rejection (ratio 10-

7)

high EUV sensitivity Highly radiation hard Chemical inertness Mechanically robust (high Young modulus) High electric charge mobility = fast response time Low dielectric constant = low capacitance

Diamond & nitrides are appealing materials for the EUV photon detection. Their main properties are hereafter sumarized :

Page 8: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Rivelatori a diamanteDevice area: 6 6 mm2 Thickness: 40 µm Grain size: 20 µmSensitive area 4 mm2

Interdigitated contacts

spacing 20 mthickness 0.1 melectrode width 15 m No thermal annealing

back contact 25 mm2

Page 9: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Dark current

-200 -150 -100 -50 0 50 100 150 200-1.4

-1.2

-1.0

-0.8

-0.6

-0.4

-0.2

0.0

0.2

0.4

0.6

0.8

1.0

1.2

1.4

Au

Voltage (V)

Cur

rent

(pA

)

Page 10: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Stabilità e risposta temporale

-200 0 200 400 600 800 1000120014001600

0

20

40

60

80 36 KV/cm

28 KV/cm

20 KV/cm

Pho

tocu

rren

t (nA

)

Time (s)

0 20 40 60 80 100 120 140 160 180 200

0,0

0,2

0,4

0,6

0,8

1,0

1,2

20 KV/cm 28 KV/cm 36 KV/cm

Nor

mal

ized

Pho

tocu

rren

t

Time (s)

Toff = 30 %

Page 11: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Quantum Efficiency

200 400 600 800 10001E-8

1E-7

1E-6

1E-5

1E-4

1E-3

0,01

0,1

1

10

100

E = 28 KV/cm

Ele

ctro

n / p

hoto

n

Wavelength (nm)

100 120 140 160 180 200 220 240 2600,01

0,1

1

10

100

1000

10000

QE Diamond QE CCD QE MCP + KBr

Qua

ntum

Effi

cien

cy (%

)Wavelength (nm)

[1] Naletto, Pace et al, 1994

[2] Wilhelm et al.,1995

[2]

[1]

Diamond efficiency Comparison with other detectors

E. Pace et al., Diam. Rel. Mater. 9 (2000) 987-993.

Page 12: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Diamond – Responsivity

-200 -150 -100 -50 0 50 100 150 200-1,2

-1,0

-0,8

-0,6

-0,4

-0,2

0,0

0,2

0,4

0,6

0,8

1,0

1,2

1,4

Voltage (V)

Cur

rent

(pA

)

Dark current @ room temperature

Vbias = 30 V

Page 13: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Our proposal: flip-chip CMOS imager

Select the most appropriate sensitive material

Exploit the advantages offered by the CMOS technology to fabricate system-on-a-chip detectors

Join the best material and on-chip CMOS electronics by means of the consolidated flip-chip technology (applied to IR photon and particle detection)

The idea

Page 14: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Diamond bump-bonded detector

Incident radiation

Open electrode

CMOS imager

Sensitive layer

Pixel array

12.5 m

Page 15: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Applicazioni attuali Applicazioni attuali

alla fisica delle particellealla fisica delle particelle

Page 16: Camera CCD in sviluppo allXUVLab per un esperimento su razzo, precursore dellesperimento UVC del Solar Orbiter Compact (72mm x 72mm x 50mm) Lightweight.

Advantages of flip-chip technology

High responsivity Visible rejection Available technologies Frame format and pixel size in the spec On-chip read-out electronics Radiation hardness Compact detector (reduced weight) Low power consumption High frame rate Windowing

EUV sensitive layers bump-bonded on CMOS imagers could have many appealing features, such as: