1 / 23

Sergio Ricciarini ~ INFN Firenze on behalf of PAMELA collaboration Vertex 2006 15 th International Workshop on Vertex D

PAMELA Silicon Tracker experience and operation. Sergio Ricciarini ~ INFN Firenze on behalf of PAMELA collaboration Vertex 2006 15 th International Workshop on Vertex Detectors Perugia, 28 September 2006. Summary. Introduction. The PAMELA experiment.

apollo
Download Presentation

Sergio Ricciarini ~ INFN Firenze on behalf of PAMELA collaboration Vertex 2006 15 th International Workshop on Vertex D

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. PAMELA Silicon Tracker experience and operation Sergio Ricciarini ~ INFN Firenze on behalf of PAMELA collaboration Vertex 2006 15th International Workshop on Vertex Detectors Perugia, 28 September 2006

  2. Summary • Introduction. • The PAMELA experiment. • The magnetic spectrometer and silicon tracker. • Detectors and read-out electronics. • Tracker performances. • Preliminary analysis of a sample of data taken in flight. • Examples of events collected in flight by PAMELA. S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  3. ITALY: •INFN Florence and Physics Department of Florence University •Istitute of Applied Physics “Nello Carrara”, Florence • INFN Bari and Physics Department of Bari University • INFN and Physics Department of Rome "Tor Vergata" • INFN Naples and Physics Department of Naples University • INFN Trieste and Physics Department of Trieste University • INFN National Laboratories, Frascati GERMANY: Physics Department of Siegen University SWEDEN: Royal Institute of Technology, Stockholm RUSSIA: • Ioffe Physico-Technical Institute, St Petersburg • Cosmic Rays Laboratory, Moscow Engineering and Physics Institute, Moscow • Lab. of Solar and Cosmic Ray Physics, P.N. Lebedev Physical Institute, Moscow S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  4. PAMELA experiment operational launch (rest) Primary production  annihilation m() = 964 GeV (Ullio 1999) Al container filled with N2 at 1 atm 2 mm thick window • Main scientific objectives: • antiparticles in cosmic rays; • search for antimatter and dark matter; • cosmic-ray propagation; • solar modulation, solar physics. • Mission overview: • on-board Resurs-DK1 Russian satellite, launched from Bajkonur (Kazakhstan) 15 June 2006; • quasi-polar orbit 70° inclination, 350-600 km altitude; • long expected duration (> 3 years);  efficient rejection of atmospheric background (albedo);  high statistics, also at lower energies (geomagnetic effect). • Design goals for PAMELA performance: S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  5. PAMELA apparatus • Main requirements: high-sensitivity antiparticle identification, precise momentum measure. • Time-Of-Flight plastic scintillator strips + PMT:  trigger, albedo rejection;  mass identification up to E ~ 1 GeV;  charge identification from dE/dX. • Magnetic spectrometer with microstrip Si tracker:  charge sign and momentum from the curvature;  charge identification from dE/dX. • Electromagnetic calorimeter W/Si sampling; 16.3 X0, 0.6 λI:  discrimination e+ / p, e- / from shower topology;  direct E measurement for e-. max diameter: 102 cm height: 130 cm weight: 470 kg power: 355 W S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  6. Bmean = 0.43 T Bmax = 0.48 T Magnetic spectrometer • Permanent magnet (5 modules): • Nd-Fe-B alloy elements, residual magnetization 1.3 T; • Al frames, tower height 44.5 cm; • geometric factor 21.5 cm2· sr; • Bx ~ Bz < 0.1 By ; • 3-axis map: 70000 points, 5 mm pitch. l a d d e r ADC boards • Tracking system (6 planes, 8.9 cm apart): • 3 independent ladders per plane: • 2 Si microstrip sensors per ladder: • double sided, with double metallization on ohmic view; • integrated capacitive coupling; • FE electronics (VA1 chips) integrated on hybrid boards. VA1 chips hybrids Si sensors S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  7. Silicon detector ladder • Sensor dimensions: 70.0 mm x 53.3 mm x 300 μm. • Read-out: • 1024 read-out channels per ladder view; • strip/electrode coupling ~ 20 pF/cm; • channel capacitance to ground: < 10 pF junction view, < 20 pF ohmic view. • Bias: • VY -VX = + 80 V fed through guard ring surrounding the strips. • Bias resistor: • junction: punch-through, > 50 MΩ; • ohmic: polysilicon, > 10 MΩ. • Leakage current < 1 μA/sensor. S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  8. VA1 chip • Main features: • 1.2 µm CMOS ASIC (CERN - Ideas, Norway); • 6.2 mm · 4.5 mm chip area; 47 μm input pad pitch; • ± 2 V power rails; • 128 low-noise charge preamplifiers; • shaping time set to 1 μs; • ± 300 mV differential output range. • Operating point: • chosen for optimal compromise; • power consumption 1.0 mW/channel  total dissipation 37 W for 288 VA1 (36864 channels); • voltage gain 7.0 mV/fC  output saturation at ~ 10 MIP. S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  9. flight data physics run physics run calibration Tracking system electronics • General characteristics: • segmentation/redundancy of power and functional sections; • devices qualified for radiation hardness (TID, SEE); • compact mechanical assembly; • limited total power consumption (63 W); • limited data bandwidth occupation (~ 10 Gbyte/day available). ADC stage: • 36 ADC sections, 1 ADC / ladder; • ADC are operated in parallel at 0.5 Msps; • event acquisition time 2.1 ms. DSP stage: • 12 DSP on 2 boards, 1 DSP/view (ADSP2187L); • control logics on FPGA chips (A54SX); • typical data compression factor 15  ~ 4 kbyte/event; • typical compression time 1.1 ms. S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  10. Tracker performances • Preliminary analysis of a sample of data taken in ~12 hours of flight. • Data show that the tracking system is working nominally as expected. • Thermal environment. • Noise performances. • Cluster multiplicity and total signal. • Signal correlation between X and Y views. • Signal/noise. • Charge discrimination capabilities. • Spatial resolution. • Momentum resolution. S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  11. Temperatures in flight • After power-up temperature remains stable: • < 1º C variations along orbit; • < 10º C difference between PAMELA off and on. • Heat from VA1 on hybrids radiated to the magnetic tower: • black IR absorbing painting on the walls; • heat released from magnetic tower to cooling loop (liquid iso-octane). At power-up: 21º C (5000 s ~ 0.9 orbits) 8 days after power-up: 28º C (10000 s ~ 1.8 orbits) S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  12. Noise in flight Noise performance is nominal, as can be seen for a typical calibration taken in flight. Y (ohmic) view has worse performance because of double metallization. Pedestal X view (DSP 6) Y view (DSP 3) flight data flight data Noise X view (DSP 6) Y view (DSP 3) flight data flight data N ~ 4 ADC counts N ~ 9 ADC counts yellow line = ground data average S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  13. Cluster characteristics flight data - preliminary flight data - preliminary flight data - preliminary one plane all planes all planes one plane Cluster inclusion cuts: S > 7 N (seed), S > 4 N (neighbours). S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  14. Signal/noise ratio Signal/noise ratio, calculated as Σ(S/N) over the cluster channels. This sample contains also non-MIP cosmic rays (He etc.). Typical average signal/noise measured at beam-test for orthogonally incident MIP: 56 (X view)26 (Y view) flight data - preliminary plane 1 S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  15. Charge discrimination flight data - preliminary He all planes beam–test data H Good H-He charge discrimination capability. magnetic rigidity R = |pc/Z| • Full charge discrimination capabilities studied with beam-test data (GSI Darmstadt, 2006). • Fragmentation of 12C projectiles on different targets (Al, polyethylene). • Single-channel saturation at ~ 10 MIP affects B-C discrimination. events average cluster signal S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  16. Spatial resolution sx = (2.77 ± 0.04) mm sy = (13.1 ± 0.2) mm Critically depends on the signal/noise ratio. Resolution for junction (X, bending) view determines the momentum measurement. Beam-test data - orthogonally incident MIP Best spatial resolution obtained with non-linear η algorithm for normally incident MIP. Resolution measurement and sensor alignment done at the last beam test of the flight model with protons of known energies (CERN SPS, 2003). Whole-tracker alignment checked with cosmic rays collected at ground level during final qualification tests (INFN Rome “Tor Vergata” laboratories, 2005). In flight: alignment parameters will be checked with high-energy electrons after collecting a sufficient statistical sample (at least 3 months of data taking). S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  17. Momentum resolution mult. scatt. spat. resol. X MDR ~ 1 TV Measured at beam test with protons of known momentum (CERN SPS, 2003). In flight cross-check with E measured by calorimeter for high-energy electrons. magnetic rigidity R = |pc/Z| magnetic deflection η = 1/R = |Z/pc| S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  18. Flight data: 10 GV electron with electr. shower S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  19. Flight data: 1.56 GV positron with electr. shower S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  20. Flight data: 36 GV proton with hadronic shower S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  21. Flight data: 18 GV antiproton without shower S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  22. Flight data: 9.7 GV He nucleus without shower S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

  23. Conclusions • PAMELA is taking data since 11 July 2006. • Up to now >900 Gbyte of data downlinked to ground. • Acquired ~ 90 · 106 events. • Apparatus operating also within radiation belts (SAA). • Magnetic spectrometer on-flight performances are nominal. • Data processing and analysis tools have been developed and used; they are now being finalized. • Next step: systematic data analysis. • Precise determination of detector characteristics. • Application to physics research items. trigger rate S. Ricciarini – PAMELA Silicon Tracker – Vertex 2006, Perugia 28 September 2006

More Related