2019
DOI: 10.1088/1748-0221/14/09/p09017
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Characterisation of a CeBr3(LB) detector for space application

Abstract: A: We describe the performance of a 23 × 23 × 30 mm 3 low background cerium bromide, CeBr 3 (LB), scintillator crystal coupled to a Hamamatsu R11265U-200 photomultiplier. This detector will be the building block for a gamma-ray detector array designed to be the payload for a CubeSat to be launched in 2020. The aim of the mission is to study flashes of gamma rays of terrestrial origin. The design of the detector has been tuned for the detection of gamma rays in the 20 keV-3 MeV energy range. K: Gamma detectors;… Show more

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Cited by 13 publications
(5 citation statements)
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“…2, center). This inorganic scintillator exhibits a light yield of 60 photons per keV, a scintillation decay time of 18 ns, a density of 5.18 g.cm −3 and a total absorption efficiency at 364 keV of 27% for a 10×10×1 cm 3 crystal block [17]. The mechanical frame is sealed with a 1.5 mm thick output glass window, which is coupled to the SiPMs array with an optical grease (BC-630, refractive index of 1.46, Saint-Gobain).…”
Section: A the Scintillator-photodetector Systemmentioning
confidence: 99%
“…2, center). This inorganic scintillator exhibits a light yield of 60 photons per keV, a scintillation decay time of 18 ns, a density of 5.18 g.cm −3 and a total absorption efficiency at 364 keV of 27% for a 10×10×1 cm 3 crystal block [17]. The mechanical frame is sealed with a 1.5 mm thick output glass window, which is coupled to the SiPMs array with an optical grease (BC-630, refractive index of 1.46, Saint-Gobain).…”
Section: A the Scintillator-photodetector Systemmentioning
confidence: 99%
“…The payload's temperature data during orbit is important to correct for detector gain drift [21], and for adjusting the operations duty cycle in flight to avoid overheating. As can be seen in the insets of figure 13, which represent the temperature recorded while the payload was operational, during a single orbit the temperature rises significantly when the payload is operating.…”
Section: Instrument Healthmentioning
confidence: 99%
“…A prototype of RAAD was built and tested at NYUAD, providing proof of concept. Details on the prototype can be found in [21]. Details on the CubeSat's bus and subsystems can be found in [22].…”
Section: Introductionmentioning
confidence: 99%
“…We propose to use a new generation of CeBr 3 scintillating crystals (Sect. 3.3.1) which have been studied to assess their suitability as spectrometer modules for space missions [70][71][72][73][74][75].…”
Section: Overviewmentioning
confidence: 99%