Title :
The BGO electromagnetic calorimeter sub-trigger electronics for DAMPE
Author :
Shanshan Gao ; Changqing Feng ; Yunlong Zhang ; Deliang Zhang ; Zhongtao Shen ; Di Jiang ; Shubin Liu ; Qi An
Author_Institution :
State Key Lab. of Particle Detection & Electron., Univ. of Sci. & Technol. of China, Hefei, China
Abstract :
The Dark Matter Particle Explorer (DAMPE) is being constructed as a scientific satellite to observe high energy cosmic rays in space. As a main sub-detector of DAMPE, the BGO electromagnetic calorimeter provides a wide measurement range of energy deposition of the particles traversing the detector and generates trigger information for the trigger selection module. There are 704 photomultiplier tube (PMT) dynode signals in total to generate the sub-trigger signals, which bring difficulties in design of the front end electronics (FEE) on the space-limited and power-limited satellite platform. To overcome the challenge, a front end ASIC chip, VATA160, which integrates 32 charge measurement channels with trigger, is adopted. There are 32 VATA160 chips mounted on 8 FEE-A boards for calorimeter. A performance test setup and a PMT calibration setup are built to evaluate the FEE-A board. The test results of RMS noise, linearity, trigger threshold and time walk effect are shown.
Keywords :
application specific integrated circuits; calibration; cosmic ray apparatus; nuclear electronics; particle calorimetry; photomultipliers; signal processing; solid scintillation detectors; trigger circuits; BGO electromagnetic calorimeter subtrigger electronics; DAMPE; Dark Matter Particle Explorer; FEE-A boards; PMT calibration setup; RMS noise; VATA160 chips; charge measurement channels; energy deposition; front-end ASIC chip; front-end electronics; high energy cosmic rays; performance test setup; photomultiplier tube dynode signals; scientific satellite; space-limited power-limited satellite platform; subtrigger signals; time walk effect; trigger information; trigger selection module; trigger threshold; Accuracy; Aerospace electronics; Charge measurement; Crystals; Delays; Noise; Satellites;
Conference_Titel :
Real Time Conference (RT), 2014 19th IEEE-NPSS
Print_ISBN :
978-1-4799-3658-8
DOI :
10.1109/RTC.2014.7097422