Detector Simulations

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Design Note TRI-DN-16-23 ALPHA-g Detector Calibration Notes
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History of Changes

Release Number	Date	Description of Changes	Author(s)
1	2016-05-31	Initial Version	Pierre Amaudruz
2	2017-02-02	Update on concept
3	2017-04-18	Update for Gate Review 3	Pierre Amaudruz Lars Martin

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Table of Figures

Figure 1 – rTPC cross-section with at the bottom the central cathode with Al strips. A laser plane illuminates the central cathode for electron production. 5

Figure 2 - Inner cylinder with copper cathode and Aluminum strips 6

Figure 3 - Optical head assembly to be mounted on the endplate 6

Figure 4 - Model of the laser equipment at the endplate with light simulated plane on first Aluminum strip. 7

Figure 5 - UBC setup for laser test 10

Figure 6 - Schematic of the UBC test configuration 10

Figure 7 - Photoemission versus incident angle for Aluminum 11

Figure 8 - Ratio of electron per photon versus incident angle for different base material 12

Purpose

The calibration system for the ALPHA-g rTPC is to provide a reference measurement of the electron drift direction and speed for a known configuration. These parameters are subject to environmental changes (pressure, temperature, gas mixture) as well as external drift voltage and magnetic field.

Method

For comparing to a reference measurement, a consistent number of primary electrons at a defined geometrical location are required. Two methods have been considered.

• Alpha source (Am241) mounted on the central cathode surface. This technique is well understood and working well in particular for a long drift detector. The emission rate from the calibration source can be adjusted but cannot be controlled. In our case, the impact of the calibration event rate on the overall physics trigger rates is to be considered as once the source are installed, the emission cannot be stopped.
• Laser beam striking aluminized surface on the central cathode to achieve electron emission. This technique has been used for the T2K TPC detector with success. The work function of the aluminum being lower than the one of copper, an increase of electron emission from the aluminum will be distinguishable relative to the copper. In our case cathode surface is copper with aluminum strips at known locations. Therefore it is possible to “image” the aluminum positions from the emitted drifting electrons to the anodes. The intended laser wavelength is to be the same as in T2K (Nd:YAG frequency-quadrupled to 266nm).

The laser method with its external trigger capability and better defined electron emission has been deemed the preferred solution.

References

Elog entry and pdf document: Laser test results by Lars Martin

Concept

The top and bottom endplates have provisions for inserting the necessary optic module to deliver a laser plane intersecting the inner cathode cylinder. The initial laser beam in the order of 0.5mm in diameter is converted into a plane through a transparent cylindrical quartz rod of 5mm diameter within the detector volume. The plane has an aperture angle in the order of 90deg illuminating both sides of the drift path. Aluminum strips on pre-defined locations along the inner cathode will emit electrons when struck by the 266nm laser light. Using a triggered pulse laser source, the electron arrival on the anode wire and the induced charge on the cathode pads along the anode wire will provide the timing and Z position of the intersection point of the aluminum strip and the laser plane. The light plane is slightly rotated and tilted off the z-axis in order separate the Al strip electron cloud from reaching all the same wires. For the given rotation and tilt angles (45deg, 1deg) we have spaced the Al strips such that 2 anode wires will be separating the 2 electron clouds of two consecutive Al strips.

Figure 1 – rTPC cross-section with at the bottom the central cathode with Al strips. A laser plane illuminates the central cathode for electron production.

Mechanical design

The mechanical modification to the endplate for the laser calibration option is minimal. They consist in:

• Placing 2 laser access holes in each endplate, giving us the option to feed 4 laser optic modules to the rTPC, see Figure 3. The advantage of multiple access points is to better cover the whole drift volume and to illuminate both ends of the detector with similar incident angles.
• Additional 9 Aluminum strips of 6mm width wrapped around the inner cylinder at 9 locations see Figure 7. Table 1 list the position of the 9 strips, the final column shows the phi coordinate at which the laser light hits the given strip for one possible set of geometric parameters of the optics package.

Strip number	Nominal z [mm]	Laser phi in degrees
0	-1060	-17.647
1	-795	-7.450
2	-530	0.447
3	-265	7.225
4	0	13.328
5	265	18.978
6	530	24.310
7	795	29.412
8	1060	34.348

Table 1 - Al strip position

Figure 2 - Inner cylinder with copper cathode and Aluminum strips

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Figure 4 - Model of the laser equipment at the endplate with light simulated plane on first Aluminum strip.

Specifications

Parameter	Value
Laser Pulsed beam	0..100Hz triggerable
Wavelength	266 nm
Power	2uW
Aluminum strip width	6mm
Aluminum strip length	Full circumference
Aluminum strip pitch in the z-direction	265mm
Number of Aluminum strips	9
Aperture angle	90 deg
Tilt angle	1 deg
Rotation angle	45 deg

Tests of the laser calibration system using the prototype show a clear pattern of the Al strips. Analysis of the pattern reproduces the strip position with good accuracy. Despite the strip pitch in the prototype being much tighter at 40mm instead of 265mm the peaks are very clearly separated in the z-pads. The amplitude variation between peaks is due to the laser intensity distribution which has not been investigated in detail. It is not a high priority because the laser system is not meant for pulse height calibration, but rather for time and position.

The laser plane is not inclined in the prototype, so a separation on the anode wires is impossible. The wider spacing for the final detector was chosen to allow for a good separation in the anodes.

As mentioned above the laser intensity distribution is not well understood yet, but we are confident we can illuminate the 4-5 strips closest to each laser port. The combination of shallow incidence angle and low geometric efficiency makes it questionable whether enough light can reach the far end of the TPC. It may be possible to increase the laser intensity to reach further strips at the expense of saturating the signals in the intensity maximum.

Appendix I – Bench tests

To reproduce the T2K laser calibration configuration in the Alpha-g rTPC, it would require shining the laser normal to the inner cathode surface. While the drift region is about 1m long for T2K, it is about 5cm in the Alpha-g. In addition the outer surface of the rTPC is fully occupied with the cathode pad readout electronics boards preventing any acceptable insertion of laser light direction normal to the tangent of its surface.

The remaining possible solution for the Alpha-g laser calibration is to shine the laser from its endplates. There the space is also quite restricted but available. In this configuration see Figure 1, the incident light angle varies from about 45 deg to less than 1deg due to the rTPC geometrical proportions. The electron emission efficiency at these incident angles varies substantially.

The shallow angle of the laser light on the central cathode cylinder is a concern for the electron emission efficiency. In order to quantify the parameter for the laser source specification, we have gone through multiple tests at UBC where a vacuum chamber with a 266nm laser was available. A dedicated mounting setup within the vacuum chamber permitted to rotate a plane holding our material sample, see Figure 2. The setup consisted in a double plate “capacitor-like” configuration, with one of the electrodes holding the sample and the other collecting the emitted electrons, see Figure 3. The signal was then collected through a dedicated DAQ for signal charge analysis versus incident angle on different material.

Figure 5 - UBC setup for laser test

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Figure 6 - Schematic of the UBC test configuration

The Aluminum and copper have different “work function” values. The results from T2K showed electron extraction from the aluminum to be about 2 pe/mm² while for copper around 0.03 pe/mm². This ratio of 70 provides the necessary contrast for strip localization and therefore local drift time calibration. Similar tests at UBC were set up to possibly confirm these numbers. In addition the work function values found in literature fluctuate sufficiently that the selected materials may overlap with a 266nm wavelength. Therefore we added to our test the target composition (Al, Cu, C) as a variable to see if a better suited material can be identified.

In the Alpha-g case, the laser incident angle is grazing the cathode surface. Hence we included in the incident angle of the laser beam on target as a variable as well (see. Figure 4). Our tests did not reproduce the T2K results. That ratio of collected electron to the estimated number of photons on target versus the photon (laser beam) incident angle is not as large as seen in T2K at normal incidence. But we did expect to see a large variation of electron emission as we move away of a normal incidence. A proposed method to recover those “missing” electron due to the grazing incident angle, was to “scratch” the surface of the target (aluminum) to have some normal area to the incident laser light (note that 90deg incident angle is normal to the surface). This is visible with the “Al scratched 2” plot (the Alpha-g incident angle range is between 0.5 and 45deg). The effect of the scratching does increase the emission at grazing angle quite substantially, which is what we were looking for.

Unfortunately it was not possible to get reasonable values comparing different target materials. It remains unclear why this is the case.

The material options for strip/cathode combinations were aluminum on copper or aluminum on carbon loaded Kapton. Both cathode materials are suitable for the rTPC. In light of the prototype results shown above it was decided to stick with the copper cathode and scratched aluminum strips.

Wavelength 266nm, Photon energy: 4.66 eV

Material	Work function (eV)
Cu	4.53 – 5.10
Al	4.06 – 4.26
C	~5

Figure 7 - Photoemission versus incident angle for Aluminum

Figure 8 - Ratio of electron per photon versus incident angle for different base material