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SPACIROC Spatial Photomultiplier Array Counting and Integrating ReadOut Chip. S. Ahmad, P. Barrillon , S. Blin , S. Dagoret , F. Dulucq , C. de La Taille IN2P3-OMEGA LAL Orsay , France Y. Kawasaki - RIKEN,Japan I. Hirokazu – JAXA, Japan. Main application: JEM-EUSO.
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SPACIROCSpatial PhotomultiplierArrayCounting and IntegratingReadOut Chip S. Ahmad, P. Barrillon, S. Blin, S. Dagoret, F. Dulucq, C. de La Taille IN2P3-OMEGA LAL Orsay, France Y. Kawasaki - RIKEN,Japan I. Hirokazu – JAXA, Japan
Main application: JEM-EUSO • EUSO-BALLOON : • Project CNES + IRAP (Toulouse), APC and LAL supported by the whole JEM-EUSO collaboration • 1 PDM with electronics and mechanics as close as possible to the one of JEM-EUSO • SPACIROC : Mapmt readout • Goals: • Launch in 2014 • Technological demonstrator (PDM + software) • Study of the background • Detection of an atmospheric shower JEM-EUSO : • Extremely High Energy Cosmic Ray (EECR) observer onboard of International Space Station • Observing Extensive Air Shower created by the EECRs • Total irradiation dose: 60 krad/5years • Launch in 2016 TWEPP 2012, Oxford
Front End ASIC requirements • 64 channels photon counting • Single photon counting 100% trigger efficiency: 1/3 pe (~50 fC when MaPMT gain=106) • Double pulse resolution : ~10 ns • => 3 different designs are embedded • Charges to Time (Q-to-T) converters (based on KI02 ASIC – JAXA/RIKEN) • 8 channels: each for 8-pixel sum preamplifier signals • Pixels charge measurement: 2pC – 200pC • Data acquisition & Readout to be done within 2.5 µs (GTU) • Readout Clock : 40MHz • Radiation Hardness By Design : TMR (Triple Module Redundancy) • Power budget : <1 mW/channel TWEPP 2012, Oxford
Global architecture TWEPP 2012, Oxford
Photon Counting - Architecture • 3 designs: Trig_PA: output directly from preamplifier → lowest dissipation • Trig_FSU : unipolar fast shaper → baseline • Trig_VFS : new optimised fast triggering shaper → fastest design • Multiplexed Trigger to Digital part • 2 x 10-bit DAC for threshold • Turn off all blocks. TWEPP 2012, Oxford
Q to T: Architecture • Time Over Threshold technique • based on a block designed by JAXA/RIKEN (called KI) • 8 channels: Each channel input is the sum of 8 consecutive preamplifier outputs • 10-bit DACs for threshold TWEPP 2012, Oxford
Digital Architecture • 8 identical digital module for Photon Counting => 8 clocking counters • 1 digital module for Q to T converters => 8 enable 40MHz counters • 9 serial links for data readout + TransmitOn signal Photon Counting Q to T conversion TWEPP 2012, Oxford
SPACIROC1 Technology: AMS 0.35µm SiGe Submitted in March 2010 Delivered: Mid-July Test: September Dimensions : 4.6mm x 4.1mm (19 mm²) Power supply: 0-3V Naked Die: 1700 chips Packaging : CQFP240 (proto) CQFP160 (Euso-balloon production): - 100 asics (yield: 85%) 4.6mm 4.1mm TWEPP 2012, Oxford 8
SPACIROC1: Trigger efficiency measurements • Photon Counting: • TrigFSU (Baseline) • Gain = 1mV/fC • Min input = 30 fC • Dispersion: 2.5 DAC unit • Trig_PA • Gain = 0.32mV/fC • Min input = 30 fC • Dispersion: 1.8 DAC unit • Trig_VFS • Gain = 1.3mV/fC • Min input = 60 fC • Dispersion: 17.7 DAC unit Trig_PA : 64 Channel Scurves Trig_FSU : 64 Channel Scurves Trig_VFS : 64 Channel Scurves TWEPP 2012, Oxford
SPACIROC1: Charge measurements 100 • Charge to Time converter • 8-pixel-sum: Input test: 1.6 – 160 pC • Simulation: charge up to 250pC • Measurements: saturation starts at 40pC KI 8-Pixel-Sum Simulations 250pC 65 KI 8-Pixel-Sum Measurements 160pC • ASIC Digital System: • Startbit, Data, TransmissionOn, Parity Bit • Data output Vhi-Vlo: 1.5V - 0V TWEPP 2012, Oxford
SPACIROC1 + MAPMT measurements Test setup: HVPS: K=1000V & Cockroft Walton MAPMT: Hamamatsu R11265-M64 MAPMT Gain: 1.106 (1p.e=0.16pC) DC LED : λ=378nm Photo Counting and Q to T counter data for input range of 1-180 p.e/GTU/pixel Photoelectron spectrum Photon Counting pile up: 25pe/GTU/pixel Q to T range:6.4 -198 pC TWEPP 2012, Oxford
SPACIROC1: Measurement summary • SPACIROC1 bugs • Power consumption: • Due to design bugs, unused component can’t be turned off. • Double pulse separation: • 10ns is never reached (due to the power dissipation) • Q to T converter: 8-pixel-sum • Linearity zone is 75% smaller than simulations • Integrated signal swing is 0.7V instead of 1.5V • Good behaviour for first prototype • Good baseline for Photon Counting • Slow Control cells & Digital modules working as expected • Will be used for EUSO-Balloon (CQFP160) TWEPP 2012, Oxford
SPACIROC2 • Technology: AMS 0.35µm SiGe • Submitted in November 2011 • Delivered in February 2012 • Dimensions : 4.6mm x 4.6mm (21 mm2) • Power supply: 0-3V • Packaging: CQFP208 (proto) • Modifications: • Trig_pa: add buffer • Trig vfs: add turn off switch • improve the discriminator • Q to T converter: integrated capacitor values changed • add a reset TWEPP 2012, Oxford
SPACIROC2: FSU Measurements: 64 channels FSU pedestals FSU 50fC Average Threshold = 67.8 DAC (1.119V); RMS = 0.8 DAC (~1.3mV) Average Threshold = 92.3 DAC (1.06V); RMS = 2.3 DAC (~3.8mV) • Large gap between the pedestals and 1/3 pe • → we can easily trig on 1/3 pe • Nice uniformity between channels (rms: 2.3DAC) TWEPP 2012, Oxford
SPACIROC2: PA Measurements: 64 channels • 50fC trigger requirement matched for all channels • (nice separation from pedestals) • Nice uniformity between channels ( rms: 1DAC) PA pedestals Average Threshold = 963.7 DAC (2.497V); RMS = 0.8 DAC (~1.3mV) PA 50fC Average Threshold = 954.6 DAC ( 2.483V); RMS = 1 DAC (~1.65mV) TWEPP 2012, Oxford
SPACIROC2: VFS Measurements: 64 channels • 50fC trigger requirement matched for all channels • (nice separation from pedestals) • Nice uniformity between channels ( rms: 3.5DAC) VFS 50fC VFS pedestals Average Threshold =81.44DAC (1.042V); RMS = 0.67 DAC (~1.1mV) Average Threshold = 112.25 DAC (1.093V); RMS = 3.48 DAC (~5.7mV) TWEPP 2012, Oxford
SPACIROC2: FSU Measurement – Ch32 Gain = 1.23 mV/fC Min Input = 20fC (<<1/3pe) 5sNoise = 7fC TWEPP 2012, Oxford
SPACIROC2: PA Measurement – Ch32 Gain = 0.563 mV/fC Min Input = 38fC (<<1/3pe) 5sNoise = 7.5fC TWEPP 2012, Oxford
SPACIROC2: VFS Measurement – Ch32 Gain = 1.18mV/fC Min Input = 20fC (<<1/3pe) 5sNoise = 8fC TWEPP 2012, Oxford
Double pulse separation FSU: 26 ns DAC value: 100 Injection=1pe * 2 Double pulse separation=26ns PA : 28ns DAC value: 950 Injection=1pe * 2 Double pulse separation=28.5ns VFS: 20ns DAC value: 120 Injection=1pe * 2 Double pulse separation=20ns TWEPP 2012, Oxford
Q to T(8-Pixel-Sum) - Linearity Discri output Discri input Poor linearity Not a problem for our application Only used to detect high signal => turn off the mapmt HV TWEPP 2012, Oxford
Measurement summary Almosteverything has been improved TWEPP 2012, Oxford
Conclusion • The best trigger design will be chosen by the collaboration • Spaciroc1 : demonstrator • Spaciroc2 : JEM-EUSO • Eliminate all power consumption problems • Improve double pulse separation • All trigger designs can be used TWEPP 2012, Oxford
SPACIROC1: Mapmt measurements Photon Counting KI Test setup: HVPS: K=1000V & Cockroft Walton MAPMT: Hamamatsu R11265-M64 MAPMT Gain: 1.106 (1p.e=0.16pC) DC LED : λ=378nm Photon Countingpileup:30p.e KI range:6.4 -198 pC TWEPP 2012, Oxford
Photon Counting – Simulations • Triggers for 80 fC input charge (1/2 pe for PMT gain =106) Trig_FSU Vth=1.2v Δt<10ns Trig_PA Vth=2.35v Δt<5ns Trig_VFS Vth=1.2v Δt<5ns TWEPP 2012, Oxford
Digital part waveform • GTU : 99% duty cycle synchronised to Readout clock falling edge • Each DataOut serial link: 66-bit data (StartBit + Counters Data + ParityBit) • TransmitOn signal active during data transmission on DataOut links TWEPP 2012, Oxford
Photon Counting – Simulations • Triggers for 160 fC input charge (1 pe for PMT gain =106) Trig_FSU Vth=1.2v Δt<10ns Trig_PA Vth=2.35v Δt<15ns Trig_VFS Vth=1.2v Δt<5ns TWEPP 2012, Oxford
KI 8-Pixel-Sum – Simulations • Input : 2.4pC – 240pC 2.4pC 11pC 52pC 240pC TWEPP 2012, Oxford
Q to T (8-Pixel-Sum) - Architecture Dt=25.15ns Discri output 201ns, 287ns,397ns, 509ns,608ns Ddata_ki=1 Dt=48.3ns Ddata_ki=2 Discri input Dt=59.8ns Ddata_ki=3 Dt=72.59ns Ddata_ki=4 TWEPP 2012, Oxford