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Calibration of diamond detectors for dosimetry in beam-loss monitoring

MetadataDetails
Publication Date2021-04-27
JournalNuclear Instruments and Methods in Physics Research Section A Accelerators Spectrometers Detectors and Associated Equipment
AuthorsG. Bassi, L. Bosisio, P. Cristaudo, M. Dorigo, A. Gabrielli
InstitutionsUniversity of Trieste, Istituto Nazionale di Fisica Nucleare, Sezione di Trieste
Citations15
AnalysisFull AI Review Included

This study details the assembly, characterization, and calibration of 28 single-crystal Chemical Vapor Deposition (sCVD) diamond detectors intended for high-radiation dosimetry and Beam-Loss Monitoring (BLM) at the SuperKEKB collider.

  • Material and Design: The sensors are sCVD diamond (4.5 x 4.5 x 0.50 mm3) with Ti+Pt+Au electrodes, packaged for extreme radiation hardness (expected lifetime dose > 10 Mrad).
  • Performance Validation: Transient-Current Technique (TCT) confirmed homogeneous charge transport properties across the sample set, yielding average electron and hole saturation velocities of 0.9 x 107 cm/s and 1.3 x 107 cm/s, respectively.
  • Optimal Operation: An optimal bias voltage of ±100 V was determined, achieving a steady-state charge-collection efficiency (CCE) close to 100%. Dark current at this bias is reliably less than 1 pA.
  • Calibration Method: A robust current-to-dose-rate calibration factor (k) was established using a 90Sr beta source and a silicon diode reference, significantly reducing systematic uncertainties related to source activity and simulation geometry.
  • Accuracy and Stability: The average calibration factor corresponds to 35 (mrad/s)/nA, determined with a relative systematic uncertainty of 8%. The detectors demonstrated stable current response (within 1-5% fluctuation) over several days of continuous irradiation.
  • Asymmetry Handling: Approximately half the sensors exhibited asymmetric Current-Voltage (I-V) profiles or hysteresis; for these, the polarity leading to current saturation was chosen for reliable operation.
ParameterValueUnitContext
Detector MaterialsCVD DiamondN/AGrown by Chemical Vapor Deposition (CVD)
Sensor Dimensions4.5 x 4.5 x 0.50mm3Face dimensions and thickness
Electrode CompositionTi+Pt+AuN/ALayered structure (100+120+250 nm thickness)
Optimal Bias Voltage±100VSelected for near 100% Charge Collection Efficiency (CCE)
Maximum Dark Current1pAMeasured at ±100 V bias
Electron Saturation Velocity (vsat)0.9 x 107cm/sAverage from TCT measurements
Hole Saturation Velocity (vsat)1.3 x 107cm/sAverage from TCT measurements
Average Ionization Energy (Eeh)13.1eVEnergy required to create one electron-hole pair
Average Calibration Factor (k)34.9(mrad/s)/nADose rate per measured current
Total Systematic Uncertainty8%Relative uncertainty on calibration factor k
Largest Uncertainty SourceCurrent Transients/Fluctuations5 %Contribution to systematic uncertainty on k
Operational Dose Rate RangeFew urad/s to hundred krad/sN/ARequired range for SuperKEKB monitoring
Detector Mass (m)37mgUsed in calculation of calibration factor F
  1. Detector Assembly and Initial QC:

    • sCVD sensors were mounted on Rogers PCBs. Inner coaxial cable conductors were soldered, and outer shields were fixed using conductive glue for mechanical stability.
    • Initial dark current measurements were performed up to ±800 V to ensure the current remained below 1 pA at the target operating voltage (±100 V).
  2. Charge Carrier Transport (TCT):

    • The Transient-Current Technique (TCT) was used to study electron and hole transport properties.
    • A collimated 241Am alpha source (5.485 MeV) was used to generate localized electron-hole pairs (penetration depth ~12 ”m).
    • Pulse shape analysis determined drift velocity and mobility as a function of the electric field, confirming homogeneous transport properties.
    • Pulse integral analysis determined the average ionization energy (Eeh), found to be 13.1 eV.
  3. I-V Profile and Stability Testing:

    • Current-Voltage (I-V) profiles were measured under continuous irradiation from a 90Sr beta source across a ±500 V range.
    • The optimal operating voltage (±100 V) was selected where the current reached a stable plateau, indicating maximum CCE.
    • For detectors showing asymmetric I-V profiles or hysteresis, the polarity leading to current saturation was chosen.
    • Current stability was monitored over several hours to days, confirming fluctuations were typically < 1% for symmetric sensors and < 5% for asymmetric sensors (at optimal polarity).
  4. Current-to-Dose Calibration (Reference Method):

    • Detectors were irradiated with a 90Sr beta source, and the signal current I(d) was measured as a function of source-detector distance (d).
    • A calibrated silicon diode was used as a reference detector, measuring Ir(d) under identical conditions.
    • The measured signal-to-reference ratio R = I(d)/Ir(d) was compared to the expected ratio Rexp, calculated via detailed FLUKA simulation, to determine the characteristic constant G.
    • The final calibration factor k was calculated using G and fundamental constants (k = F/G), resulting in an average value of 35 (mrad/s)/nA with 8% systematic uncertainty.

The characterized sCVD diamond detectors are suitable for applications requiring extreme radiation hardness, high stability, and precise dose rate measurement:

  • High-Energy Physics (HEP) Accelerators:
    • Beam-Loss Monitoring (BLM) and machine protection systems in colliders (e.g., SuperKEKB, LHC).
    • Dosimetry for sensitive detector components operating in high-background environments.
  • Medical Dosimetry:
    • High-precision measurement of absorbed dose in complex radiation fields (e.g., proton, heavy ion, or photon therapy).
    • Micro-dosimetry due to diamond’s tissue-equivalent properties and small active volume.
  • Nuclear and Reactor Monitoring:
    • In-situ radiation monitoring in nuclear facilities where high neutron and gamma fluxes necessitate radiation-hard sensors.
  • Space Radiation Monitoring:
    • Dosimetry for satellites and spacecraft, leveraging diamond’s stability and resistance to displacement damage in long-duration missions.
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