About  |  Board  |  Contact

NICA/MPD, JINR


HIDE MENU
SHOW MENU

NICA-MPD Detectors Subsystems

  • All systems
  • FS-A

  • Central Detector
  • FS-B
General Info
Technical info
Operating principle
Photos
Literature

NICA Multi Perpose Detector

The MPD apparatus has been designed as a 4π spectrometer capable of detecting of charged hadrons, electrons and photons in heavy-ion collisions at high luminosity in the energy range of the NICA collider. To reach this goal, the detector will comprise a precise 3-D tracking system and a high-performance particle identification (PID) system based on the time-of-flight measurements and calorimetry. The basic design parameters has been determined by physics processes in nuclear collisions at NICA and by several technical constrains guided by a trade-of of efficient tracking and PID against a reasonable material budget. At the design luminosity, the event rate in the MPD interaction region is about 6 kHz; the total charged particle multiplicity exceeds 1000 in the most central Au+Au collisions at √sNN = 11 GeV . As the average transverse momentum of the particles produced in a collision at NICA energies is below 500 MeV/c, the detector design requires a very low material budget. The general layout of the MPD apparatus is shown in Fig. 1. The whole detector setup includes Central Detector (CD) covering ±2 units in pseudorapidity (η) .


Fig. 1: A general view of the MPD detector with end doors retracted for access to the inner detector components. The detector consist of three major parts: CD-central detector, and (FS-A, FS-B) - two forward spectrometers (optional). The following subsystems are drawn: superconductor solenoid (SC Coil) and magnet yoke, inner detector (IT), straw-tube tracker (ECT), time-projection chamber (TPC), time-of-flight system (TOF), electromagnetic calorimeter (EMC), fast forward detectors (FFD), and zero degree calorimeter (ZDC).

The aim of this Project is to build a first stage of the MPD setup, which consists of the superconducting solenoid, Time-Projection Chamber (TPC), barrel Time-Of-Flight system (TOF), Electromagnetic Calorimeter (ECal), Zero-Degree Calorimeter (ZDC) and Fast Forward Detector (FFD).

The layout of the first stage MPD is shown in Fig.3. The whole Central Detector (CD) will be a 9 m long cylinder of about 6,6 m in diameter. The cross-sectional view of the MPD Central Detector is shown in Fig. 2.


Fig. 2: Cutaway side view of the Central Detector of MPD with based dimensions.

Fig. 3: Cutaway side view of the Central Detector of MPD on the first Stage.

General Info
Technical info
Operating principle
Photos
Literature

FS-A

The FS’s are optional detectors which necessity will be defined after the CD became operational and first physics data are available. Those spectrometers should provide good momentum resolution and particle identification in the intermediate rapidity interval and large momentum region. There are considered two FS’s - A and B, allocated symmetrically along the beam line. Below we present some arguments in favor of forward spectrometers.

The particle momentum resolution of stand-alone CD in the region of pseudorapidity of η > 2 is deteriorated dramatically due to small value of ∫ Bdl. The information on the particle time-of-flight with hypothesis of particle type can allow for momentum reconstruction. It is evident that as longer time-of-flight base as better particle momentum determination. The result of such approach is presented in Fig. 1. However for pions the resolution is poor even with long TOF bases. The solution of the problem could come with introduction of magnetic spectrometer. The estimation of the momentum resolution of the magnetic spectrometer shows that if coordinate accuracy of track detectors is about 200 µm and track length in magnetic field is about 1 meter that allow momentum resolution better than 2%:

∆p/p = (σ/Lp2)(pp/0.2998B) p [720/(m + 6)].

m = 5 – number of measurements along the track

B = 1 T, σ = 200 µm, L = 1 m, p = 1 GeV/c ∆P/P ~ 1.7%


Fig. 1: Momentum resolution of protons, kaons and pions defined with the TOF system.
ParameterValue
etha coverage(2.0–3.0) or (5–14) degree
magnet typeair toroid
nominal magnetic field1 T
spectrometer Z position(7600–9800) mm
B × L1 T × M
number of coordinate layers10(2 × 5) layers
spatial resolution≤ 200 µm
track efficiencyabout 99%
radiation length of layersless than 5%
particles rate106 (average – 100 Hz/cm2, near beam pipe up to 1 kHz/cm2)
sensitive areaabout 14 m2 per layer, 280 m2 in total

1. link

General Info
Technical info
Operating principle
Photos
Literature

Accelerating Magnet

1. link

General Info
Technical info
Operating principle
Photos
Literature

Lenses and Magnet

1. link

General Info
Technical info
Operating principle
Photos
Literature

Coils

1. link

General Info
Technical info
Operating principle
Photos
Literature

TM Tracker

1. link

General Info
Technical info
Operating principle
Photos
Literature

Time of Flight system

Ambitious physics goals of MPD require excellent particle identification capability over as large as possible phase space volume. Identification of charged hadrons (PID) at intermediate momenta (0.1–2 GeV/c) is achieved by the time-of-flight (TOF) measurements which are complemented by the energy loss (dE/dx) information from the TPC and IT detector systems.

The basic requirements to the TOF system are:

– large phase space coverage |η| <2;

– high granularity to keep the overall system occupancy below 10–15% and minimize efficiency degradation due to double hits;

– good position resolution to provide effective matching of TOF hits with TPC tracks;

– high combined geometrical and detection efficiency (better than 80%);

– identification of pions and kaons with 0.1 < pt < 2 GeV/c;

– identification of (anti)protons with 0.3 < pt < 3 GeV/c;

– TOF detector elements must function in a 0.5 T magnetic field.


Fig. 1: Mass separation with TOF (100 ps resolution). The green lines show boundaries for efficiency and contamination estimation.

1. link

General Info
Technical info
Operating principle
Photos
Literature

Central Detector

1. link

General Info
Technical info
Operating principle
Photos
Literature

CPC Tracker

A conceptual design of the CPC of EC Tracker is shown in Figs. 2.110,2.111. The precise coordinate determination is based on the center of gravity measurement of induced on several neighbor pads charge. The inherent precision of the CPC comes from the lithographic process used in the etching of the pad structure. With this technique the pad position can be determined with a precision of about 15 µm.

The basic elements for the CPC construction are a module panels. The procedure of module construction as follow:

— the high modulus skins of Carbon Fiber Composite (CFC) glued on both sides of 10 mm thick core of ROHACELL 31 HF [271] foam;

— to ensure the sealing of the gas box and its electrical shielding and grounding, a thin laminate of Kapton and Aluminium will be added to both sides of the panel;

— the FR-4 printed boards with cathode pad structure will be glued after that to both sides of the panel;

— at each end of the module panel, an insert will be glued, sandwiched between the two CFC.

Precision holes in the insert will permit the alignment of the panels during the detector - module assembly and provide the interface to the support system.


Fig. 1: Layout of an CPC cathode pad structure in ϕ.

Fig. 2: Layout of an CPC cathode pad structure in R.
Number of panels per chamber4 pc
Module panel thickness10 mm
Number of gaps per chamber3
Gaps2 x 5 mm
Maximum outside diameter1060 mm
Frame width30 mm
Inner diameter240 mm
Coordinate planes6 (3 R,3 ϕ)
Wires per chamber400 x 3
Wire diameter30 mkm
Wire pitch2.5 mm
Number of pads in R36 x 32 x 3 = 3456
Number of pads in ϕ320 x 3 x 3 = 2880
Chamber thickness70 mm
Space angle per chamber0.16
Total material per chamber in active area0.028 X0
Maximum number of charge particle per plane100
Occupancyless than 6%

1. link

General Info
Technical info
Operating principle
Photos
Literature

Cryostat

To obtain the assured thermal stabilization of the conductor, the cold mass is to be installed in the space between inner and outer cryostat vacuum shells and supported by high thermal resistance ties and struts. The coil is indirectly cooled by two-phase liquid helium flowing through an aluminum cooling tube, which is welded to the outside surface of the support cylinder. The cold volume is surrounded by the thermal shield supported from the side of the vacuum chamber, which is cooled by helium gas at 40-80 K.

The cryostat is equipped with radiation shield inserted between the coil and the cryostat outer can. The shield surface is covered by high purity aluminum foil to reduce radiation heat loads. About 30 layers of superinsulation separate the vacuum vessel walls from the shields. The data of the thermal load at the thermal shield multiplied by the safety factor 2 are presented in Table 2.8. The overall heat load at the level 77 K is expected not to exceed 734 W in the operational mode.

Inner radius (warm bore), m2.0
Outer radius, m2.3
Length, m5.7

1. link

General Info
Technical info
Operating principle
Photos
Literature

SC Coil

1. link

General Info
Technical info
Operating principle
Photos
Literature

ECal

The whole barrel part of MPD electromagnetic calorimeter will be constructed from 48 sectors (Fig.1). The heat-producing electronics will be thus separated from the modules and mounted on the upper parts of sectors.

Fig. 1: ECAL detector.

1. link

General Info
Technical info
Operating principle
Photos
Literature

FD Tracker

Main aims of the FFD are fast determination of a nucleus-nucleus interaction in the center of the MPD setup. Besides, there are some additional important tasks where FFD is a useful instrument. It can much help in adjustment of beam-beam collisions in the center of the MPD and operative control of the collision rate and interaction point position during a run.

In comparison with experiments at ultra-relativistic energies at RHIC and LHC, there are two essential difficulties at the NICA energies. First, the charged particles produced in collisions mainly are not relativistic, and there is a large spread of spectator velocities which differ from the velocity of light (the beam velocities are in an interval 0.78 ≤ β ≤ 0.98). Second, the particle multiplicity is much lower than one in the other collider experiments. As a result, for efficient trigger we need to cover a large acceptance and try to detect all particles with β ∼1 to achieve needed timing. It leads to conclusion that the trigger and timing detectors used in other experiments at higher energies are not an optimal solution in our case and do not allow to reach the requirements mentioned above. So, one has to develop another conception of trigger and timing detectors for the MPD experiment.


Fig. 1: Front view of FFD array (left) and module structure (right).

There is a well-known fact that central and semi-central collisions of two heavy nuclei at relativistic energies are characterized by multiple pion production. The neutral pions immediately decay with generation of many high energy photons passing the MPD subdetectors. The main idea of the FDD is to register a part of these photons at small angles to beam axis as the most suitable secondaries with highest and constant velocity. The proposed FFD design is a granulated Cherenkov detector which has a high efficiency for the high energy photons and for ultra-relativistic charged particles as well. The FFD consists of two sub-detectors, FFD-L and FFD-R, which are symmetrically placed to the MPD center along the beam line. Each sub-detector array has a hole for the beam pipe and locates at a distance of 75 cm from the center. Its acceptance in pseudo-rapidity is 2.5 ≤| η |≤ 3.2.

1. link

General Info
Technical info
Operating principle
Photos
Literature

Solenoid Poles

1. link

General Info
Technical info
Operating principle
Photos
Literature

Straw EC Tracker

1. link

General Info
Technical info
Operating principle
Photos
Literature

Time of Flight system

Ambitious physics goals of MPD require excellent particle identification capability over as large as possible phase space volume. Identification of charged hadrons (PID) at intermediate momenta (0.1–2 GeV/c) is achieved by the time-of-flight (TOF) measurements which are complemented by the energy loss (dE/dx) information from the TPC and IT detector systems.

The basic requirements to the TOF system are:

– large phase space coverage |η| <2;

– high granularity to keep the overall system occupancy below 15% and minimize efficiency degradation due to double hits;

– good position resolution to provide effective matching of TOF hits with TPC tracks;

– high combined geometrical and detection efficiency (better than 90%);

– identification of pions and kaons with pt < 1.5 GeV/c;

– identification of (anti)protons with pt < 3 GeV/c;

– TOF detector elements must function in a 0.5 T magnetic field.


Fig. 1: Mass separation with TOF (100 ps resolution). The green lines show boundaries for efficiency and contamination estimation.
At the relatively high momenta of particles the errors in time of flight measurement and track length definition have higher weight than the error of momentum determination. The momentum spectra of secondary particles at the NICA colliding energies produced in the regions of pseudorapidity |η| < 1.2 and 1.2 < |η| < 2 for minimum (4 GeV) and maximum (11 GeV) colliding energies are presented on the Fig. 2. The average momentum of pions for energy 4 GeV is about 300 MeV/c and for 11 GeV is about 400 MeV/c.

Figure 2: Momentum spectra of pions, kaons and protons in two regions of pseudorapidity: |η| < 1.2 (left) and 1.2 < |η| < 2 (right) and for two center of mass energy: 4 GeV (top) and 11 GeV (bottom).
The smallest track length for time of flight measurement at MPD is 1.5 m. We expect to have overall time resolution better than 100 ps. It allows us reliable separation of pions, kaons and protons in the entire interval of momenta for produced particles for NICA energies (Fig. 3a, 3b).

Figure 3a: Calculation of the separation of pion and kaons in units of standard deviation as a function of TOF base for TOF resolutions: 80ps and 100 ps. Figure 3b: Separation of pions and kaons as a function of secondary particles momenta for different fixed bases (time resolution is 100 ps).
In Fig. 4 we present the fraction (in percent) of pions and kaons below a particular momentum as a function of momentum. These distributions are obtained for the particle spectra. One may conclude that TOF system can separate pions on the level of 99 % and kaons – almost 98 % up to the total momentum of 1.5 GeV/c.

Figure 4: Part of the pions and kaons below a particular momentum (√(SNN)= 9 GeV).
Main parameters of the TOF system parts are listed in Table 1. Calculated total sensitive area of the TOF system is about 50.3 m2. The inner radius of the barrel is about 1.45 m. The total area of a dodecahedron with this inner radius and length of 5.7 m is about 53 m. It means estimated geometrical efficiency must be about 95%.
 Number of detectorsNumber of readout stripsSensitive area, m2Number of FEE cardsNumber of FEE channels
MRPC1240.2205248
Module61441.0812288
Sector245764.19481152
Barrel288691250.357613824
(1728 chips)
Table 1: Main parameters of the TOF system

After analyzing the results of testing of prototypes we have fixed the design and geometry of the MRPC for barrel TOF. It will be double stack MRPC with strip readout. Detail layout of the MRPC for MPD time-of-flight system A scheme of the MPD TOF detector is presented in Fig. 1. The detector consists of two stacks of 5 gas gaps each. As resistive electrodes we use common float glass. The outer glass electrodes have thickness 0.55 mm. The internal glass electrodes have thickness 0.4 mm. The fishing line as a spacer defines the 220 μm gap between all resistive electrodes. The outer part of external glass electrodes is covered by conductive paint with surface resistivity about 2 – 10 MΩ/□ to apply high voltage. All internal glasses are floating. The pickup electrodes look like strips and made on the PCB board (Fig. 3.2). An important feature of the double-stack “strip” prototype is that the internal strips of two different stacks are separated by 5-mm panel of Honeycomb. This ensures the symmetry between two stacks, and provides the equal speed of signals on the anode and cathode strips and as result prevent the dispersion of the signal.

Figure 1: Sectional view of the proposed double stack strip MRPC for TOF MPD.

Figure 2: PCB board with 10 mm wide strips.
Dimension of active area of one MRPC is 300 x 735 mm2. It has 24 readout strips, 10 mm wide and 735 mm long. To reduce crosstalk the gap between strips is 2.5 mm. Thus the pitch of electrodes in this case is 12.5 mm. Active surface of one strip is about 90 cm2. Mean occupancy for this area (see Fig. 1.8) not exceed 17 % for central Au-Au collisions with energy √(S_NN )= "11" "GeV" . Differential analog signal is transferred from PCB by twisted pair cable to front-end electronics. Signal is reading out from both ends of the strip. It provides better time resolution and determination of the coordinate of a particle along strip. For stiffening structure we glue aramid fiber honeycomb panel with a thickness of 8 mm on outer part of the external PCBs.

Figure 3: The main sizes of TOF barrel in φ direction
The cylindrical part of ToF MPD located in the barrel between the time-projection chamber (TPC) and the electromagnetic calorimeter (ECal). The TOF system internal diameter is 2.89 m from the beam axis and outer diameter is 3.41 m (Fig. 1). The MPD ToF covers the pseudorapidity range |η| ≤ 1.2 and full coverage in φ. The total surface of the barrel TOF system is about 53 m2. The TOF detector system is organized in a modular way in order to minimize the number of components and cost. The detector is segmented in φ into 12 sectors of ~5.7 m length. The maximum distance between sectors does not exceed 15 mm. Each sector carries 4 individual modules (Fig. 2). Each module contents 6 MRPCs arranged in 2 layers. The special shape of module minimizes the dead area inside the sector. The dead area between sectors is due to the limited space along the radius of barrel. This fact is not allows to put modules with overlap azimuthally dire. Each ToF module consists of a two separate volumes: inner gas region which contains the six MRPCs and an outer one containing the Front End Electronic (FEE) cards, cables, high voltage and gas plugs. The MRPCs have been described in detail in Chapter 2. The inner gas tight box containing the MRPCs is made of the polypropylene trough 5 mm thick and the polypropylene cover same thick with the holes to bring the MRPCs signals to the Interface Cards (IC), where the FEEs will be plugged into and the FEEs themselves. Holes for gas connectors and HV connectors are also provided on the top cover. The MRPCs are positioned inside the box as shown in Fig. 2.

Figure 4: Modules along beam direction
Adjacent MRPCs will be positioned inside the module in such a way as to create an overlap of 4 readout strips between two adjacent MRPCs, at the edge of the active area: this will ensure the inter-calibration of the MRPCs via tracks traversing both of them. The signals from the pick-up strips on the MRPCs are brought to the FEE via Interface Cards (ICs). The ICs are made of small PCBs and will be glued and fixed to the top cover of the box closing in this way the gas volume. Each IC will have on one side the connectors facing the MRPC, and, on the other side, the connectors for the FEEs. To add safety to the system the perimeter of the IC is poured silicone.

Figure 5: Pair of modules on one aluminum frame
Two modules are combined in pairs on one aluminum frame (Fig. 3). A lid of aluminum honeycomb closing in this way the volume for the electronics and the cables covers the frame. Two pair of modules are inserted into the frame of barrel from each side of the barrel forming one sector. The cables taking the signals from FEE to the TDC readout modules will be routed to the center of the module and from there to the readout crates placed at both ends of each sector. At the present time two sample TOF modules are made for tests (Fig. 6). We use it for optimization of the overall design of the all TOF system.

Figure 6: MRPCs inside the gas volume of the module (left). TOF module on the cosmic stand (right).

Figure 1: Time of Flight (ToF) mass separation (identification)
The MRPC is a stack of resistive glass plates. A high voltage is applied to the external surfaces of the stack. Further out there are pickup electrodes. A charged particle ionizes the gas and the high electric field amplifies this ionization by an electron avalanche. The resistive plates stop the avalanche development in each gap; they are however transparent to the fast signal induced on the pickup electrodes by the movement of the electrons. So the total signal is the sum of the signals from all gaps (the reason for many gaps is to achieve high efficiency), whereas the time jitter of the signal depends on the individual gap width (the reason for narrow gaps is to achieve good time resolution).

Figure 2: Principle of operation of Multigap Resistive Plate Chamber (MRPC)
  • Cosmic test setup
  • 24-channel amplifier based on NINO with VHDCI output connector
  • Readout from two stacks of the MRPC
  • Test beam MPD
  • Time-to-digital converter TDC72VHL
  • TOF Electronics for data acquisition system
  • MRPC prototype in positioning device
  • TOF MRPC assembling
  • Detectors assembling and cosmic test together with young scientists from Bulgaria
  • Nuclotron beamtest with two Chinese groups

1. MPD NICA. Technical Design Report of the Time of Flight System (TOF) Laboratory of High Energy Physics, JINR, Dubna — V.A. Babkin, S.N. Bazylev, M.G. Buryakov, V.M. Golovatyuk, P.O. Dulov, D.S. Egorov, Yu.I. Fedotov, V.I. Kolesnikov, S.P. Lobastov, V.A. Petrov, M.M. Rumiantcev, V.M. Slepnev, I.V. Slepnev, A.V. Shutov, A.V. Shipunov, S.V. Volgin, N.M. Vladimirova,

General Info
Technical info
Operating principle
Photos
Literature

Time projection chamber

The MPD time projection chamber (TPC) is the main tracking detector of the central barrel and, together with the internal tracking system, time of flight system and electromagnetic calorimeter has to provide charged particles momentum measurement with sufficient resolution, particle identification and vertex determination, two track separation and dE/dx measurement for hadronic and leptonic observables at pseudorapidities |η| <1.2 and pt >100 MeV/c.

The electromagnetic calorimeter will provide, in conjunction with the data from the TPC, reliable electron identification to study dielectron processes. TPC has to provide the high dE/dx resolution in the high multiplicity environment of a Au + Au central collision to identify electrons with an efficiency of over 90% and reject pions at the level of 103.

The track reconstruction in the region of pseudorapidity beyond 1.2 is provided by both TPC and End cap straw tracker. In order to have excellent momentum resolution and identification capability in this region the end plate elements of the TPC and readout electronics which is mounted on them have to be minimized for material budget. Thus material budget of endplate and readout electronics is about 15%. The requirements to the TPC performance following from the physics described above are as follows:

— provide efficient tracking up to pseudorapidity region |η| =1.2.

— the momentum resolution for charge particles about 2% at the transverse momentum of 300 Mev/c.<.p>

— the two-track resolution has to be about 1 cm in order to provide interference measurements with a resolution in relative momentum of a few MeV/c.

— for hadron and lepton identification a dE/dx resolution better than 8% is desirable


Fig. 1: Schematic view of the MPD TPC
ItemDimension
Length of the TPC340cm
Outer radius110cm
Inner radius27cm
Outer radius of the drift volume100cm
Inner radius of the drift volume35cm
Length of the drift volume150cm (of each half)
CathodeMembrane at the center of the TPC
Electric field strength~140 V/cm
Magnetic field strength0.5 Tesla
Drift gas90% Ar+10% Methane at Atmospheric + 2 mbar
Drift velocity5.45 cm/µs
Drift time~ 28µs
Transverse diffusion230 µm/√
cm at magnetic field0.5 Tesla
Longitudinal diffusion360 µm/√ cm
Number of readout chambers24 (12 per end plate)
Multiplisity (central collision)~ 800
Number of pads~ 80000
Pad numbers after zero suppression< 10%
Pad size4x10 mm in inner sector area
6×12 in outer sector area
Spatial resolutionσz ~ 1 mm, σx ~ 0.6 mm, σy ~ 0.8 mm
∆E/dX resolution~ 8% (75 samples× 2 cm)
Maximum rate~ 5 − 6 kHz (Lum. 102cm−2s−1)
Electronics shaping time~180 ns (FWHM)
Signal to noise ratio20:1
Signal dynamical range10 bits
Sampling rate12.5 MHz
Sampling depth350 time buckets

1. link

General Info
Technical info
Operating principle
Photos
Literature

Supporting rings

1. link

General Info
Technical info
Operating principle
Photos
Literature

Yokes

The Solenoid iron yoke is a cylindrical steel structure consisting of 12 flux return bars, two supporting end rings, two pole tips and support structures. The 6 m long flux return bars are trapezoidal in cross-section, and weigh 17.2 ton each. They form the barrel part of the yoke, which contains the cryostat with the superconducting coil.

The supporting rings have a 4 m I.D., 5.34 m incircle O.D. and twelve chord surfaces on the 4.8 m diameter to control the azimuth and radial location of each flux return bar, with an axial thickness of 270 mm. A support ring weighs 20.9 ton each. Each pole piece weighs 28.4 ton and is fixated relative to the supporting ring. They have a conical 14 grad inner diameter, whole axial thickness 600 mm, a 3.9 m O.D. and a recess on the inner face surface for the trim coil. A 50 mm annular gap between supporting ring inner diameter and pole piece outer diameter is provided for passage of cables and tubing of internal detectors. To simplify manufacturing and transportation the poles are divided in axial direction on two parts consolidated by bolts which weigh about 14 ton each.

The solenoid support structure consists of two cradles weighing 17.5 ton each. They embrace the five lower flux return bars of the yoke barrel part. The support structure is placed on a transport carriage guided by two rails. The magnet traveling section (the magnet without both poles) can be moved between experimental hall and assembly area as required.

Two pole piece support structures weighing 31.7 tons each rest on rails so that the poles may be withdrawn to provide access to the ends of internal detector elements. All magnet yoke material is specified as Steel 10 which has a minimum yield strength of 210 MPa with an annealed heat treatment.

The magnetic field quality required that deflections in the magnet structure are to be minimized to less than 1 mm. This can be accomplished with precise fabrication of magnet components and the use of high strength bolted and pinned connections between mating components.

Yoke supports have to fixate the magnet at the foundation rigidly and to provide adjustment of the detector systems relative to the beam axis. To minimize the yoke deformations, five bottom beams will be welded-in to the yoke supports.

Incircle radius of the yoke, m2.4
Circumcircle radius of the yoke, m2.67
Distance between pole tips, m5.24
Length of the yoke, m6.4

1. link

General Info
Technical info
Operating principle
Photos
Literature

Zero degree calorimeter tracker

The events classification by centrality of the relativistic nuclei collisions is a key topic of the experiments studying a strongly excited (hot and/or dense) hadronic matter properties. Obviously, the selection of central events is a necessary to study the most excited nuclear matter. However centrality classification not only separates central and peripheral events. Observables analysis in different centrality intervals appears very informative and allows to study space–time picture of the nuclear–nuclear collisions as well as hadronic matter properties, both of which impossible without centrality data involving. The importance of centrality classification can be illustrated by the following examples:

• The ratio of the elliptic flow to the space excentricity of the collision region is a constant for a wide range of the impact parameter, as it obtained at the RHIC experiments [273]. This fact as well as a great value of elliptic flow is a strong experimental indication for a small (≤ 1fm/c) thermalization time value. Such measurements are impossible without centrality classification of events, because space excentricity of the collision region is determined by centrality.

• For description of the Jet Quenching and J/Ψ suppression in nuclei–nuclei collisions the nuclear modification factor (RAA) is used. This factor depend from the number of binary collisions, which is determined by centrality.

Many examples of another observables, which requires centrality classification too, can be presented. However lets only note, that many current and planned relativistic nuclei collision experiments are paid essential attention to centrality extraction topics as well as measurements of the observables dependence on centrality (see and references in it).


Fig. 1: Front view of ZDC. The squares size is 5 × 5 cm2

1. link

General Info
Technical info
Operating principle
Photos
Literature

Cradles

1. link

General Info
Technical info
Operating principle
Photos
Literature

IT Gem

1. link

General Info
Technical info
Operating principle
Photos
Literature

IT Gem

1. link

General Info
Technical info
Operating principle
Photos
Literature

IT Tracker

1. link

General Info
Technical info
Operating principle
Photos
Literature

Gem Tracker

1. link

General Info
Technical info
Operating principle
Photos
Literature

FS-B

The FS’s are optional detectors which necessity will be defined after the CD became operational and first physics data are available. Those spectrometers should provide good momentum resolution and particle identification in the intermediate rapidity interval and large momentum region. There are considered two FS’s - A and B, allocated symmetrically along the beam line. Below we present some arguments in favor of forward spectrometers.

The particle momentum resolution of stand-alone CD in the region of pseudorapidity of η > 2 is deteriorated dramatically due to small value of ∫ Bdl. The information on the particle time-of-flight with hypothesis of particle type can allow for momentum reconstruction. It is evident that as longer time-of-flight base as better particle momentum determination. The result of such approach is presented in Fig. 1. However for pions the resolution is poor even with long TOF bases. The solution of the problem could come with introduction of magnetic spectrometer. The estimation of the momentum resolution of the magnetic spectrometer shows that if coordinate accuracy of track detectors is about 200 µm and track length in magnetic field is about 1 meter that allow momentum resolution better than 2%:

∆p/p = (σ/Lp2)(pp/0.2998B) p [720/(m + 6)].

m = 5 – number of measurements along the track

B = 1 T, σ = 200 µm, L = 1 m, p = 1 GeV/c ∆P/P ~ 1.7%


Fig. 1: Momentum resolution of protons, kaons and pions defined with the TOF system.
ParameterValue
etha coverage(2.0–3.0) or (5–14) degree
magnet typeair toroid
nominal magnetic field1 T
spectrometer Z position(7600–9800) mm
B × L1 T × M
number of coordinate layers10(2 × 5) layers
spatial resolution≤ 200 µm
track efficiencyabout 99%
radiation length of layersless than 5%
particles rate106 (average – 100 Hz/cm2, near beam pipe up to 1 kHz/cm2)
sensitive areaabout 14 m2 per layer, 280 m2 in total