Characterisation of a CeBr3(LB) detector for space application

A. Di Giovanni; L. Manenti; F. Alkhouri; L. R. Alkindi; A. Almannaei; A. Al Qasim; M. L. Benabderrahmane; G. Bruno; V. Conicella; O. Fawwaz; Prashanth Marpu; P. Panicker; C. Pittori; M. S. Roberts; T. Vu; F. Arneodo

doi:10.1088/1748-0221/14/09/P09017

Characterisation of a CeBr₃(LB) detector for space application

A. Di Giovanni
, L. Manenti
, F. Alkhouri
, L. R. Alkindi
, A. Almannaei
, A. Al Qasim
, M. L. Benabderrahmane
, G. Bruno
, V. Conicella
, O. Fawwaz
, Prashanth Marpu
, P. Panicker
, C. Pittori
, M. S. Roberts
, T. Vu
, F. Arneodo

Research output: Contribution to journal › Article › peer-review

16 Scopus citations

Abstract

We describe the performance of a 23 × 23 × 30 mm³ low background cerium bromide, CeBr₃(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.

Original language	British English
Article number	P09017
Journal	Journal of Instrumentation
Volume	14
Issue number	9
DOIs	https://doi.org/10.1088/1748-0221/14/09/P09017
State	Published - 20 Sep 2019

Keywords

Gamma detectors (scintillators, CZT, HPG, HgI etc)
Photon detectors for UV, visible and IR photons (vacuum) (photomultipliers, HPDs, others)
Scintillators and scintillating fibres and light guides
Scintillators, scintillation and light emission processes (solid, gas and liquid scintillators)

Access to Document

10.1088/1748-0221/14/09/P09017

OpenUrl availability

Full text

Cite this

Giovanni, A. D., Manenti, L., Alkhouri, F., Alkindi, L. R., Almannaei, A., Qasim, A. A., Benabderrahmane, M. L., Bruno, G., Conicella, V., Fawwaz, O., Marpu, P., Panicker, P., Pittori, C., Roberts, M. S., Vu, T., & Arneodo, F. (2019). Characterisation of a CeBr₃(LB) detector for space application. Journal of Instrumentation, 14(9), Article P09017. https://doi.org/10.1088/1748-0221/14/09/P09017

@article{44e6b324ec3c4f4fbe5273dd446ebec8,

title = "Characterisation of a CeBr3(LB) detector for space application",

abstract = "We describe the performance of a 23 × 23 × 30 mm3 low background cerium bromide, CeBr3(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.",

keywords = "Gamma detectors (scintillators, CZT, HPG, HgI etc), Photon detectors for UV, visible and IR photons (vacuum) (photomultipliers, HPDs, others), Scintillators and scintillating fibres and light guides, Scintillators, scintillation and light emission processes (solid, gas and liquid scintillators)",

author = "Giovanni, \{A. Di\} and L. Manenti and F. Alkhouri and Alkindi, \{L. R.\} and A. Almannaei and Qasim, \{A. Al\} and Benabderrahmane, \{M. L.\} and G. Bruno and V. Conicella and O. Fawwaz and Prashanth Marpu and P. Panicker and C. Pittori and Roberts, \{M. S.\} and T. Vu and F. Arneodo",

note = "Funding Information: One major mission to study TGFs has already begun in 2018 with the installation of the ASIM (Atmosphere-Space Interactions Monitor) on the CEPF (Columbus External Platform Facility) of the ISS [26]. Another mission should start at the end of 2019 with the launch of TARANIS (Tool for the Analysis of Radiation from lightning and Sprites), a satellite designed to specifically observe TGFs and related atmospheric phenomena [27]. The RAADSat would be one of the first satellites built on a low-budget to study TGFs. The mission, whose cost is about half a million USD, is supported by the U.A.E. Space Agency through the 2018 “U.A.E. Minisat Competition”, where the proposed payload has won the first place and has been awarded 100k USD. Publisher Copyright: {\textcopyright} 2019 IOP Publishing Ltd and Sissa Medialab.",

year = "2019",

month = sep,

day = "20",

doi = "10.1088/1748-0221/14/09/P09017",

language = "British English",

volume = "14",

journal = "Journal of Instrumentation",

issn = "1748-0221",

publisher = "Institute of Physics",

number = "9",

}

Giovanni, AD, Manenti, L, Alkhouri, F, Alkindi, LR, Almannaei, A, Qasim, AA, Benabderrahmane, ML, Bruno, G, Conicella, V, Fawwaz, O, Marpu, P, Panicker, P, Pittori, C, Roberts, MS, Vu, T & Arneodo, F 2019, 'Characterisation of a CeBr₃(LB) detector for space application', Journal of Instrumentation, vol. 14, no. 9, P09017. https://doi.org/10.1088/1748-0221/14/09/P09017

TY - JOUR

T1 - Characterisation of a CeBr3(LB) detector for space application

AU - Giovanni, A. Di

AU - Manenti, L.

AU - Alkhouri, F.

AU - Alkindi, L. R.

AU - Almannaei, A.

AU - Qasim, A. Al

AU - Benabderrahmane, M. L.

AU - Bruno, G.

AU - Conicella, V.

AU - Fawwaz, O.

AU - Marpu, Prashanth

AU - Panicker, P.

AU - Pittori, C.

AU - Roberts, M. S.

AU - Vu, T.

AU - Arneodo, F.

N1 - Funding Information: One major mission to study TGFs has already begun in 2018 with the installation of the ASIM (Atmosphere-Space Interactions Monitor) on the CEPF (Columbus External Platform Facility) of the ISS [26]. Another mission should start at the end of 2019 with the launch of TARANIS (Tool for the Analysis of Radiation from lightning and Sprites), a satellite designed to specifically observe TGFs and related atmospheric phenomena [27]. The RAADSat would be one of the first satellites built on a low-budget to study TGFs. The mission, whose cost is about half a million USD, is supported by the U.A.E. Space Agency through the 2018 “U.A.E. Minisat Competition”, where the proposed payload has won the first place and has been awarded 100k USD. Publisher Copyright: © 2019 IOP Publishing Ltd and Sissa Medialab.

PY - 2019/9/20

Y1 - 2019/9/20

N2 - We describe the performance of a 23 × 23 × 30 mm3 low background cerium bromide, CeBr3(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.

AB - We describe the performance of a 23 × 23 × 30 mm3 low background cerium bromide, CeBr3(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.

KW - Gamma detectors (scintillators, CZT, HPG, HgI etc)

KW - Photon detectors for UV, visible and IR photons (vacuum) (photomultipliers, HPDs, others)

KW - Scintillators and scintillating fibres and light guides

KW - Scintillators, scintillation and light emission processes (solid, gas and liquid scintillators)

UR - https://www.scopus.com/pages/publications/85074292076

U2 - 10.1088/1748-0221/14/09/P09017

DO - 10.1088/1748-0221/14/09/P09017

M3 - Article

AN - SCOPUS:85074292076

SN - 1748-0221

VL - 14

JO - Journal of Instrumentation

JF - Journal of Instrumentation

IS - 9

M1 - P09017

ER -