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11
The X-HPD: Development of a large spherical hybrid photodetector
A. Braem +, C. Joram +, J. Séguinot +, L. Pierre *, P. Lavoute *
+ CERN, Geneva (CH) * Photonis SAS, Brive (F)
Introduction: C2GT, requirements, Hybrid tubes
The X-HPD concept
Proto 0: A first sealed prototype with metal anode
Proto 1: Towards a full X-HPD
Summary and Outlook
22
e, ,
CC reactionsin H2O
segmented photosensitive ‘wall’about 250 × 250 m2
Fiducial detectormass ~ 1.5 Mt
(E below threshold for production)
~ 50 m
e±, ± 42°Che
renk
ov lig
ht
Cherenkov light
Principle of neutrino detection by Cherenkov effectin C2GT (CERN To Gulf of Taranto)
The wall is made of ~600 mechanical modules (10 x 10 m2), each carrying 49 optical modules.
10
m
A. Ball et al., Eur. Phys. J. C (2007)
33
The ideal photodetector for C2GTThe ideal photodetector for C2GT
• large size (>10”)
• spherical shape, must fit in a pressure sphere
• ± 120° angle of acceptance
• optimized QE for 300 < < 600 nm
• single photon sensitive
• timing resolution 1-2 ns
• no spatial resolution required
• electronics included
• cost-effective (need ~32.000 !)
• adapted to industrial fabrication
120°
42°
44
432 mm
(17”)380 mm
PAHV
optical gel(refr. index matching + insulation)
benthos sphere(432 / 404)
electrical feed-throughsvalve
standard base plate of HPD 10” (prel. version).
C2GT Optical Module
15
joint Si sensor
ceramic support
55
Concept of a spherical tube with central spacial anode
• Radial electric field negligible transit time spread ~100% collection efficiency no magnetic shielding required
• Large viewing angle (d ~ 3)
• Possibility of anode segmentationimaging capability (limited!)
• Sensitivity gain through ‘Double-cathode effect’
T ~ 0.4 QE
QE
66
Silicon is a good anode material for a HPD
• Gain = e·UC-A / 3.6 eV ~ 5000 for 20 kV
• Back scattering rel. small BS = 0.18 (20 kV)
• However: large tube requires large Si sensor
large capacitance (35 pF/cm2)
ns timing only with segmented sensor (few pF)
Scintillator as alternative anode ? Readout by conv. PMT.• Idea is not new ! Philips SMART tube, Lake Baikal QUASAR tube.
Pad HPD
Single padS/N up to 20
1 p.e.
2 p.e.
3 p.e.
Viking VA3 chip (peak = 1.3 s, 300 e- ENC)UC = -26 kV
both tubes used thindisks of P47 phosphor (YSO:Ce powder)Philips made
~30 tubes(1980s-1992)
200 tubesin operation since 1998
77
PMTXP2982
pressure sphere
The Philips SMART Tube The QUASAR 370 Tube
G. van Aller et al. A "smart" 35cm Diameter Photomultiplier. Helvetia Physica Acta, 59, 1119 ff., 1986.
gprimary ~ 35, t ~ 2.5 ns / Npe
R. Bagduev et al., Nucl. Instr. Meth. A 420 (1999) 138
88
SMART and Quasar tubes were the first X-HPDs
• however the use of a disk shaped scintillator didn’t allow to exploit full potential.
• need to use fast scintillator, e.g. cube or cylinder.
• Require• high light yield high gain• short decay time• Low Z preferable low back scattering coefficient • Emission around = 400 nm
LY (LY ( / keV / keV nsns ZZeffeff BSBS emissionemission (nm) (nm)
YAP:CeYAP:Ce 1818 2727 3232 ~0.35~0.35 370370
LYSO:CeLYSO:Ce 2525 ~40~40 6464 ~0.45~0.45 420420
LaBrLaBr33:Ce:Ce 6363 3030 4747 ~0.4~0.4 360360
LaBr3 is quite hygroscopic
• side and top require conductive and reflective coating define el. potential, avoid light leaking out.
• Problem: crystals have high refr. index (~1.8) large fraction of light is trapped inside crystal due to total internal refection.
99
X-HPD ½ scale prototype (208 mm Ø)
LYSO 12 Ø × 18 mm
1010
Electrostatics (SIMION 3D)
Expected performance• Viewing angle 120°• X-tal hit probability ~ 100%• flight time spread ~0.4 ns (RMS)
Simulation (SIMION 3D). 1/2 scale prototype. electron flight time
0
1
2
3
4
5
6
7
8
0 30 60 90 120
polar angle (degr.)
flig
ht t
ime
(n
s)
mean = 6.1 nsTTS = 0.37 ns (RMS)
Can be furtherimproved by optimizingbulb geometry.
1111
First build a HPD with metal-cube anode (1 cm3)‘Proto 0’
0
10
20
30
40
50
60
300 350 400 450 500 550 600
(nm)
QE
(%
)
0
0.5
1
1.5
2
2.5
3
ratio
QE top QE side
Built in CERN plant.
0
0.2
0.4
0.6
0.8
1
1.2
-180 -135 -90 -45 0 45 90 135 180
f,q (degrees)
rel.
sen
sitiv
ity
f
q
measured at Photonis
A. Braem et al., NIM A 570 (2007) 467-474
1212
Prepare and characterize components for real X-HPD ‘Proto 1’
PMTPhotonis XP3102 (25 mm Ø)
electrical feedthrough Al coated
1313Calibration: 1 p.e. = 0.0514·109 Vs
ENF ~ 1.15
PMT XP3102 has verygood signal properties.
1414
Test set-up
Lab e- accelerator
based on pulsedphotoelectronsfrom a CsI cathode.
DAQ on digital scope.LeCroy Waverunner LT344.
vacuum pump (turbo)P < 10-5 mbar
Pulsed H2 flash lamp(VUV)
MgF2
sapphirewindow
mirror
-UPC = 0 -30 kV
collimator
CsI photocathode
X-HPD anode
1515
PM T pulse (LYSO, Ee = 20 keV)
-100
-80
-60
-40
-20
0
20
-50 0 50 100 150 200 250
time (ns)
pu
lse
he
igh
t (m
V) data
fit (45 ns)
Pulse shape on scope.
Contributions from individual photoelectrons clearly visible
1616
Charge amplitude
for single photoelectrons… and multi-photoelectrons
modest photo counting ability
1717
0
5
10
15
20
25
30
0.0 5.0 10.0 15.0 20.0 25.0 30.0
U (kV)
N p
.e.
0.0
0.2
0.4
0.6
0.8
1.0
Rel
. Lig
ht O
utpu
t
LYSOdata
rel. light output of LSO (literature)
fit (relative light output)
Calibration of charge amplitude (for single incident photoelectrons) using single photon response of PMT
= primary gain of X-HPD
1818
LYSO, Ee = 27.5 keV
Fit = Gauss + Exp.
Wrote a very simple M.C.:
Ingredients: BS + E’e spectrum + statistics
Input: <Np.e.>, Poisson
e-
BS BS
Ee
E’e lost ?
PMT
e- back-scattering from LYSO
Single photoelectron spectra are well described by Gaussian + Exponential.
Where does the non-Gaussian part come from ?
Ee-E’e
E.H. Darlington, J. Phys. D, Vol. 8 (1975) 85
Expect to loose <10% of single photoelectrons by a 3 pedestal cut.
single p.e. detection efficiency of X-HPD ~90%
1919
What happens to back scattered electrons in radial E-field of X-HPD ?• Low energy electrons (E < 5 keV) are reabsorbed within << 1 ns.• For E > 5 keV re-absorption (within ~1 ns) or loss. Depends on hit position and
emission angle.
X-tal top
X-tal side
2020
First photoelectron timing
y = 8.03x-0.47
y = 36.40x-0.42
1.5
1.61.7
1.8
1.92
2.1
2.2
2.32.4
2.5
12.5 15 17.5 20 22.5 25 27.5 30
U (kV)
RMS
time
reso
l. (n
s)
8
8.5
9
9.5
10
10.5
11
11.5
12
time
(ns)
LYSO crystal
Timing studies with first electron method
clock start clock stop
2121
Include time calculation in M.C. Needed 1 ns overall jitter to describe data.
M.C. shows stronger tails than actually measured, because all BS electrons are assumed to be lost.
2222
Summary and Outlook
X-HPD • is an attractive concept for
large area photodetection• promises higher
performance than classicalPMT
• proof of principle OK• components characterized
Next steps• Make X-HPD with LYSO
X-anode in ~2-3 weeks• Test it at CERN and at
Photonis + …• Improve light extraction
from LYSO crystal. Ideas exist.
2323
Back-up Transparencies
2424
• Ee = 25 keV - 0.5 keV (E-loss in Al layer) × 25 ph/kev (scint. yield)
612 ph
• d/4 = 0.16(qcrit = 33.5°) 98 ph
• Fresnel reflection losses ~ -10% 90 ph
• <QE> ~ 0.25 22.5 p.e.
X-tal with Al coating
MgF2 anti-reflection coating at exit side
Window (+ opt. grease)
Light guide (Al coated)
PMT window (+ opt. grease)
Photocathode
Estimate of the photoelectric yield
2525
LSO crystal with PMT readout. The plot shows the reconstructed number of photoelectrons as function of the applied voltage at the CsI cathode. Full and open symbols correspond to UPMT = 1000 V and 900 V, respectively. The fits to the data are explained in the text. The relative light output of LSO [15][16] is shown as dashed line (secondary axis).
0
5
10
15
20
25
30
35
40
45
0.0 10.0 20.0 30.0U (kV)
N p
.e.
0.0
0.2
0.4
0.6
0.8
1.0
Re
l. L
igh
t Ou
tpu
t LSO
YAP
rel. light output (LSO)
A. Braem et al., NIM A 570 (2007) 467-474
Crystals coupled via sapphire window to PMT. Use of optical grease.
2626LSO crystal read out with PMT. As previous figure, however the light intensity of the flash tube was increased. On average there is about 1 photoelectron. The pedestal peak is cut at 250 counts.
A. Braem et al., NIM A 570 (2007) 467-474
LSO crystal coupled via sapphire window to PMT. Use of optical grease.
2727
PhotonisXP 1807
PhotonisXP 1806
PhotonisXP 1805
PhotonisXP 1804
q ~ 30° q ~ 35°q ~ 35°
q ~ 35° q ~ 31° q ~ 31°
2828
CERN CERN photocathode photocathode ‘transfer’ plant ‘transfer’ plant