report from trd workshop trento, march 3-4 results from test beam analyses tr–production and...
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Report from TRD WorkshopTrento, March 3-4
results from test beam analysesTR–production and X-ray absorption
measurementsgas properties recent advances of the read out electronicsprogress on DCS and services super-module design and integration status of chamber production software statusplanning
Hannes Wessels, Univ. Muenster
Test Beam Setup at T10
measurements w/omagnetic field
measurements withmagnetic field
Test Beam Setup Setup with 4 small chambers and a prototype of
the largest TRD chamber (1200x1600mm2) (DC5)
Cleanliness of e/ Separation
with coincidencesof the two Cherenkovcounters-> contaminationof e in and viceversa smaller than1/1000
V. Yurevich, A. Andronic
Performance of Various Radiators
-> no significant momentum dependence of -rejection
A. Andronic
Charge Distributions
-> distributions well described at fixed momenta-> possible effect of Bremsstrahlung visible
A. Andronic
e/ – Performance by Layer
-> performance of individual layers almost identical-> slight improvement with depth (Bremsstrahlung)-> slightly worse performance for large prototype (S/N)
A. Andronic
Independence of Efficiencies
-> efficiencies for pion identification of the different layers factorize
-> layer 5 slightly worse due to different S/N
A. Andronic
Influence of Material in Front of TRD
-> performance of the different layers with (triangles) and w/o (circles) material in front of the radiator
-> 8mm Al -> X/X0~9%
-> 10cm in front of DC1
-> small impact at very low momenta
A. Andronic
Influence of Material on Resolution
-> B=0-> no effect on resolution for pions-> small effect for e
O. Busch
Influence of Material on Resolution
-> B=0, 0.28, 0.42, 0.56 T
-> no change in resolution for pions
-> electrons somewhat affected as depth increases because Bremsstrahlung is produced before dipole
O. Busch
Position and Angular Resolution
-> no deterioration of resolution in magnetic field
-> slight decrease in angular resolution for large angles -> space charge effects
O. Busch
Lorentz Angle Measurements
-> good agreement of data and simulation to the level that CO2
contents variation, drift velocity, and alignment are understood
O. Busch
TR Measurements
-> beam is deflected from TR photon by B-field
O. Busch
Energy and Multiplicity of TR Photons
-> TR energy spectrum well understood-> measured multiplicity lower than simulated ~0.85
O. Busch
X-Ray Absorption Measurements
Setup at MPI Heidelberg
R. Schicker, T. Lehmann
Measurements of Radiator Materials
-> actual radiator less than 50% transparency for ETR < 6keV
R. Schicker, T. Lehmann
Gas Property Measurements
using mini-drift chamber establish procedure of known
mixtures (Ar/CO2, Ar/CH4) then test Xe-based mixtures (Xe/CO2, Xe/CH4)
G. Tsiledakis, C. Garabatos
l=2.25 cm
d=3.15 cm
Slit1 Slit2
90Sr (-source)
drift region
pads A KScintillator (trigger) phototube
drift electrode
Ua=1.5 kV
Ud=-1 kV -1.3 -1.6 : : -3.7
t1 t2
t=t2-t1
E=Ud/d (kV/cm) /p(bar)
u=l/t (cm/s)
Drift velocity measurements small DC
gas-mixturepads along pads
across pads
G. Tsiledakis, C. Garabatos
pad number
Drift time (s)
PH
(m
V/0
.74 )
Ar-CO2 (23%) gas mixture
E (kV/cm)
Dri
ft v
eloc
ity
(cm
/s)
GARFIELD
along pads
across pads
Why 23% CO2? New calibration of the flow meters
Test of the method shows agreement with GARFIELD
All next measurements “across pads”
G. Tsiledakis, C. Garabatos
Ar-CH4 (10%) gas mixture
E (kV/cm)
Dri
ft v
eloc
ity
(cm
/s)
GARFIELD
MIT measurements
2nd GSI measurements
1st GSI measurements
First runUse of a premixed gas mixture shows a discrepancy with GARFIELD and MIT .Second runRe-mixing on our own after a new calibration.Confirms MIT measurements, GARFIELD, our calibration and our method.
G. Tsiledakis, C. Garabatos
Xe-CH4 (10%) gas mixture
E (kV/cm)
Dri
ft v
eloc
ity
(cm
/s)
GARFIELD
MIT Christophorou
GSI
Disagreement with Garfield and measured data!
G. Tsiledakis, C. Garabatos
Xe-CO2 (15.4%) gas mixture
GARFIELD
GSI
Disagreement with Garfield
Dri
ft v
eloc
ity
(cm
/s)
E (kV/cm)
G. Tsiledakis, C. Garabatos
Xe-CO2 (20.5%) gas mixture
GARFIELD
GSI
Disagreement with Garfield
Dri
ft v
eloc
ity
(cm
/s)
E (kV/cm)
-> need certainty about gas composition
-> multiple scattering in Xe larger?
-> existing data insufficient
-> need measurements with controlled nitrogen contamination
G. Tsiledakis, C. Garabatos
Gas system statusGas system statusC. Garabatos, GSIC. Garabatos, GSI
• stability of pressurestability of pressure• NN22 separation separation• membrane testmembrane test
Stability of detector pressure
-0.5 -0.4 -0.3 -0.2 -0.10
10
20
30
40
50
60
70
P = -0.30 ± 0.03 mbar
En
trie
s
Overpressure (mbar)
C. Garabatos, GSIC. Garabatos, GSI
Concerns about cryogenics method
For on-line regeneration: Long regeneration times: several weeks Safety: lack of NL2 would result in loss of gas and
perhaps loss of the plant Need extra Xe volumes Composition gets modified Consider, for the filling, the use of membranes
(Fill with CO2, not with N2) During running periods, leaks must be kept to a
minimum Use cryogenics only at end-of-run is desirable
C. Garabatos, GSIC. Garabatos, GSI
Semi permeable membrane test(from ATLAS TRT)
CO2-enriched
Gas in
Permeate out(CO2)
Polyamide capillary tubes
C. Garabatos, GSIC. Garabatos, GSI
Performance expectationsfor one TRD filling
Pressure
(bar)
Xe lost (m3)
Time (days)
Xe lost(m3)
Time (days)
1 2 6.5 1.3 6.5
2 2 4.5 1.0 4.5
3 2 3.5 0.9 3.5
4 2 2.8 0.8 2.8
1 membrane 2 membranesC. Garabatos, GSIC. Garabatos, GSI
Summary
N2 removal feasible at end-of-run
Also possible on-line, but long and tedious
membranes look attractive for the filling (with CO2)
last crucial test (gas distribution) are being carried out right now
PRR after PRR of ATLAS TRT No document à la TPC foreseen
C. Garabatos, GSIC. Garabatos, GSI
The leak question
0
10
20
30
40
50
0 0.2 0.4 0.6 0.8 1Absolute leak rate (l/h)
ppm
or k
€/ye
ar [O2] (ppm)
money (k€/year)
Leak rate 0.27 l/hReg. Flow = leak rate
0
1
2
3
4
5
0 50 100 150 200 250
time (days)[N
2 ] (%
)
C. Garabatos, GSIC. Garabatos, GSI
Electronics Progress
PASATRAP – ADC, digital filter, tracklet
pre-processor, tracklet processor, controls
read out boardDCSgrounding services
PASA - Chip
Parameter
No. channels 18+3
Noise (ENC) 702 e (25pF)20e/pF
Conversion Gain
12.5 mV/fC
Shaping time about 120 ns
Non-linearity < 0.16%
Power consumption
13.5 mW/ch
output variationswith T, Vdda
<0.23% (20 deg)<0.03% (200mV)
-> fully differential design
-> essentially ready for submission (end of April)
-> final simulations in conjunction with ADC ongoing
-> potential problem with ground loop under investigation
H.K. Soltveit, V. Catanescu
Measured Crosstalk as Function of Pad-Pad Capacitance
max. input signal
crosstalk in %
H.K. Soltveit, V. Catanescu, I. Rusanov
ADC
10bit, 10MHz cyclic converter designed by University of Kaiserslautern
current design needs 0.1mm2 and 6mW needs additional input buffer for decoupling from
PASA no longer providing reference voltages to PASA potential ground loop because input cells also
need analog 3.3V full design with 21 channels will be part of the
next submission (May)
D. Muthers, R. Tielert, KL
ADC Chip Performance
490
500
510
520
530
540
Input amplitude 100 mV, 576 samples
AD
C o
utpu
t
0 100 200 300 400 500
-2
0
2
RMS=0.869 for timebins>99
RE
S
Timebin
- ADC tested with all CPUs running and IRQs turned on- ADC power derived from digital power and turned on from idle state (unrealistic worst case)- observed drift less than 1 bit- rms deviation from fit to pure sine wave < 0.9 bit
V. Angelov, HD
Tracklet Preprocessor
DFIL
Event Buffer
Condition Check
DFIL Event Buffer
DFIL
Event Buffer
Condition Check
DFIL
Event Buffer
Condition Check
DFIL Event Buffer
DFIL
Event Buffer
Condition Check
Qhit
hit
Qhit
Qhit
18+1 channels
COGPosition
CalcLUT
Para-meterCalc
Hit
Sel
ectU
nit (
max
. 4 h
its)
PositionCalcLUT
Para-meterCalc
PositionCalcLUT
Para-meterCalc
PositionCalcLUT
Para-meterCalc F
IT R
egis
ter
Fil
e an
d tr
ackl
et s
elec
tion
CPU0
CPU1
CPU2
CPU3
C
RL
A
AACOG
Q
COG
COG
COG
ADC
ADC
ADC
ADC
ADC
ADC
Non-Lin
Offs Tail-canc
Gain Cross-talk
Digital FILter64 timebins deep
FIT register file is for the CPUs a readonly register file
V. Angelov, HD
Pedestal correction (offset)
This filter stage corrects for some offset in PASA and ADC and adds a programmable offset to the corrected value
V. Angelov, HD
Tail cancellation filter
This filter stage corrects for the gas ion tail. It is a IIR filter. The tail can be approximated
by a sum of two exponentials.
The parameters are selected with the requirements: output pulse has nearly Gaussian shape and no undershoot.
V. Angelov, HD
Summary of Test Results
What has been tested :Serial Configuration, most of the configuration registers in all blocks, connected to the Global Bus;Clock gating, Global State Machine;The large LUTs (non-linearity, position), Event Buffers;CPUs with Register Files and Interrupt controllers;DFF Instruction and Quad Port Data Memories, Quad Port Full Custom Instruction and Data Memories;Local Buses;parallel Network outputs with the delay units;Acquisition in the event buffers, digital filters;ADCs;PLL, Clock and Pretrigger distribution outputsparallel Network inputs
What is still not tested : Real acquisition mode
V. Angelov, HD
Summary of Test Results
many functional bugs - none of them makes the chip unusable. For final version they are not acceptable
-> simulate !CPUs operate at clocks up to 70-80 MHz,
instead of 120MHz. Some parts operate reliably up to 120MHz (SCSN, GSM). -> timing analysis !
The ADC parameters (noise and some bad effects at large amplitudes) are not influenced by switching the CPUs on
V. Angelov, HD
Read Out Boards
-> one board for all layers
I. Rusanov, HD
MCM BoardsI. Rusanov, HD
-> designed as BGA
-> direct chip-to-chip bonding
-> version with PASA, ALTRO, and TRAP chip still needs to be evaluated
Noise Measurements on Large PrototypeI. Rusanov, M. Ciobanu, T. Mahmoud
-> frequency response of PASA on the bench
Noise Measurements on Large PrototypeI. Rusanov, M. Ciobanu, T. Mahmoud
-> typical response without good shielding/grounding
Noise Measurements on Large PrototypeI. Rusanov, M. Ciobanu, T. Mahmoud
-> response with current shielding/grounding concept
TRD DCS Card
one card per chamber DIMM connector contains TTC FPGA running Linux Ethernet network multiplexed ADC inputs for monitoring T,V etc. needs about 5W
DCS board ---> KIP software ---> Worms
M. Stockmeier, V.Petracek, D. Gottschalk
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
SupermoduleSupermodule
Length: 7mLength: 7mWeight: ~ 300kgWeight: ~ 300kgFully equipped: ~ 1,2 toFully equipped: ~ 1,2 to
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
New chamber segmentationNew chamber segmentation
• 12 different chamber types12 different chamber types• Largest ROC 1,45m x 1,2mLargest ROC 1,45m x 1,2m• Only 2 differnt types per Only 2 differnt types per
layerlayer
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
SupermoduleSupermodule
TOFTOF
TRD SMTRD SM
Rail-roller systemRail-roller system
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
SupermoduleSupermodule„2/5“ Prototype„2/5“ Prototype
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
SupermoduleSupermoduleservice spaceservice space
-> space for services very tight
-> 4mm reduction of chamber width on both sides
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
SupermoduleSupermoduleRail SystemRail System
Fixed railFixed rail movable railmovable rail
To avoid additional load from the space frameTo avoid additional load from the space frame
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
Supermodule into LDSSupermodule into LDS
•Handling and transport frameHandling and transport frame
•Lifting deviceLifting device
•supermodulesupermodule
ALICE-TRD Workshop, 3.3. – 4.3.03, TrentoALICE-TRD Workshop, 3.3. – 4.3.03, Trento Bernd Windelband, Uni HeidelbergBernd Windelband, Uni Heidelberg
Lifting deviceLifting device(LDS)(LDS)
Readout Chambers
dimensions frozen new pad plane backing currently evaluating with
two large chambersassembly proceduretoolingtest procedureleak tightnessgain uniformitytolerances
PRR April,30 ready for production in
Heidelberg starting in May
Drift volume
Radiator
Padplane/Read out unit
Side frame
H. Appelshaeuser, D. Emschermann, T. Mahmoud
Assembly of TRD Chambers
- clean room- 3D measurement system- precision mounting jigs
Chamber + Radiator
Radiator Production in Münster
all fiber material ordered material cut for largest
modules backing on order from
AIK and Fischer 3 glass tables ready
can work on 2 radiators/table
tools in preparationdone for first radiators
assembly of 6 radiators in parallel
neglecting man power2 radiators ready / day
D. Bucher, W. Verhoeven
Deformations of Wire Grids after Wiring
-> well within acceptable tolerances
H. Appelshaeuser
Wire Spacing After Wiring
-> without (!) combs for wire alignment
H. Appelshaeuser
Wire Tension Measurements
cathode anode
-> deformation due to cathode as expected; no effect on anode
D. Emschermann
Pad Planes
designs for all chambers almost finished
alternating tilted pads designwill have identical footprint on
readout sideforesee NO connector on pad plane,
instead use Z-bonding tape for direct connection of cable to read out board
D. Emschermann
Software Developments
framework well advancedneeds implementation/parameterization of
actual TR response for PID simulationneeds implementation of services trigger simulation ongoing along with
hardware implementation scheme
NEED backward compatibility of AliROOT
General Planning
would like to initiate integration meeting with TOF and technical coordination
will aim for re-baselining of the detector after PRR of chambers and submission of digital chip (catch up during production)