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A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance
The Educational Irish Research Satellite 1 (EIRSAT-1) is a 2U CubeSat being developed under ESA’s Fly Your Satellite! programme. The project has many aspects, which are primarily educational, but also include space qualification of new detector technologies for gamma-ray astronomy and the detection...
Autores principales: | , , , , , , , , , |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
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Springer Netherlands
2021
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8556213/ https://www.ncbi.nlm.nih.gov/pubmed/34744308 http://dx.doi.org/10.1007/s10686-021-09779-9 |
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author | Murphy, David Ulyanov, Alexey McBreen, Sheila Doyle, Maeve Dunwoody, Rachel Mangan, Joseph Thompson, Joseph Shortt, Brian Martin-Carrillo, Antonio Hanlon, Lorraine |
author_facet | Murphy, David Ulyanov, Alexey McBreen, Sheila Doyle, Maeve Dunwoody, Rachel Mangan, Joseph Thompson, Joseph Shortt, Brian Martin-Carrillo, Antonio Hanlon, Lorraine |
author_sort | Murphy, David |
collection | PubMed |
description | The Educational Irish Research Satellite 1 (EIRSAT-1) is a 2U CubeSat being developed under ESA’s Fly Your Satellite! programme. The project has many aspects, which are primarily educational, but also include space qualification of new detector technologies for gamma-ray astronomy and the detection of gamma-ray bursts (GRBs). The Gamma-ray Module (GMOD), the main mission payload, is a small gamma-ray spectrometer comprising a 25 mm × 25 mm × 40 mm cerium bromide scintillator coupled to an array of 16 silicon photomultipliers. The readout is provided by IDE3380 (SIPHRA), a low-power and radiation tolerant readout ASIC. GMOD will detect gamma-rays and measure their energies in a range from tens of keV to a few MeV. Monte Carlo simulations were performed using the Medium Energy Gamma-ray Astronomy Library to evaluate GMOD’s capability for the detection of GRBs in low Earth orbit. The simulations used a detailed mass model of the full spacecraft derived from a very high-fidelity 3D CAD model. The sky-average effective area of GMOD on board EIRSAT-1 was found to be 10 cm(2) at 120 keV. The instrument is expected to detect between 11 and 14 GRBs, at a significance greater than 10σ (and up to 32 at 5σ), during a nominal one-year mission. The shape of the scintillator in GMOD results in omni-directional sensitivity which allows for a nearly all-sky field of view. |
format | Online Article Text |
id | pubmed-8556213 |
institution | National Center for Biotechnology Information |
language | English |
publishDate | 2021 |
publisher | Springer Netherlands |
record_format | MEDLINE/PubMed |
spelling | pubmed-85562132021-11-04 A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance Murphy, David Ulyanov, Alexey McBreen, Sheila Doyle, Maeve Dunwoody, Rachel Mangan, Joseph Thompson, Joseph Shortt, Brian Martin-Carrillo, Antonio Hanlon, Lorraine Exp Astron (Dordr) Original Article The Educational Irish Research Satellite 1 (EIRSAT-1) is a 2U CubeSat being developed under ESA’s Fly Your Satellite! programme. The project has many aspects, which are primarily educational, but also include space qualification of new detector technologies for gamma-ray astronomy and the detection of gamma-ray bursts (GRBs). The Gamma-ray Module (GMOD), the main mission payload, is a small gamma-ray spectrometer comprising a 25 mm × 25 mm × 40 mm cerium bromide scintillator coupled to an array of 16 silicon photomultipliers. The readout is provided by IDE3380 (SIPHRA), a low-power and radiation tolerant readout ASIC. GMOD will detect gamma-rays and measure their energies in a range from tens of keV to a few MeV. Monte Carlo simulations were performed using the Medium Energy Gamma-ray Astronomy Library to evaluate GMOD’s capability for the detection of GRBs in low Earth orbit. The simulations used a detailed mass model of the full spacecraft derived from a very high-fidelity 3D CAD model. The sky-average effective area of GMOD on board EIRSAT-1 was found to be 10 cm(2) at 120 keV. The instrument is expected to detect between 11 and 14 GRBs, at a significance greater than 10σ (and up to 32 at 5σ), during a nominal one-year mission. The shape of the scintillator in GMOD results in omni-directional sensitivity which allows for a nearly all-sky field of view. Springer Netherlands 2021-08-13 2021 /pmc/articles/PMC8556213/ /pubmed/34744308 http://dx.doi.org/10.1007/s10686-021-09779-9 Text en © The Author(s) 2021 https://creativecommons.org/licenses/by/4.0/ Open AccessThis article is licensed under a Creative Commons Attribution 4.0 International License, which permits use, sharing, adaptation, distribution and reproduction in any medium or format, as long as you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons licence, and indicate if changes were made. The images or other third party material in this article are included in the article's Creative Commons licence, unless indicated otherwise in a credit line to the material. If material is not included in the article's Creative Commons licence and your intended use is not permitted by statutory regulation or exceeds the permitted use, you will need to obtain permission directly from the copyright holder. To view a copy of this licence, visit http://creativecommons.org/licenses/by/4.0/ (https://creativecommons.org/licenses/by/4.0/) . |
spellingShingle | Original Article Murphy, David Ulyanov, Alexey McBreen, Sheila Doyle, Maeve Dunwoody, Rachel Mangan, Joseph Thompson, Joseph Shortt, Brian Martin-Carrillo, Antonio Hanlon, Lorraine A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance |
title | A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance |
title_full | A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance |
title_fullStr | A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance |
title_full_unstemmed | A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance |
title_short | A compact instrument for gamma-ray burst detection on a CubeSat platform I: Design drivers and expected performance |
title_sort | compact instrument for gamma-ray burst detection on a cubesat platform i: design drivers and expected performance |
topic | Original Article |
url | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8556213/ https://www.ncbi.nlm.nih.gov/pubmed/34744308 http://dx.doi.org/10.1007/s10686-021-09779-9 |
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