Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads
Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for ad...
Ausführliche Beschreibung
Autor*in: |
de Kuijper, Kees [verfasserIn] Diwan, Rishank [verfasserIn] Pal, Partha Sarathi [verfasserIn] Ritter, Andreas [verfasserIn] Parkinson, Pablo M. Saz [verfasserIn] Kong, Andy C. T. [verfasserIn] Parker, Quentin A. [verfasserIn] |
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Format: |
E-Artikel |
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Sprache: |
Englisch |
Erschienen: |
2024 |
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Schlagwörter: |
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Anmerkung: |
© The Author(s) 2024 |
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Übergeordnetes Werk: |
Enthalten in: Experimental astronomy - Springer Netherlands, 1989, 57(2024), 2 vom: 23. März |
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Übergeordnetes Werk: |
volume:57 ; year:2024 ; number:2 ; day:23 ; month:03 |
Links: |
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DOI / URN: |
10.1007/s10686-024-09936-w |
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Katalog-ID: |
SPR055263712 |
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520 | |a Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. | ||
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650 | 4 | |a Astrophotonics |7 (dpeaa)DE-He213 | |
700 | 1 | |a Diwan, Rishank |e verfasserin |4 aut | |
700 | 1 | |a Pal, Partha Sarathi |e verfasserin |4 aut | |
700 | 1 | |a Ritter, Andreas |e verfasserin |4 aut | |
700 | 1 | |a Parkinson, Pablo M. Saz |e verfasserin |4 aut | |
700 | 1 | |a Kong, Andy C. T. |e verfasserin |4 aut | |
700 | 1 | |a Parker, Quentin A. |e verfasserin |4 aut | |
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10.1007/s10686-024-09936-w doi (DE-627)SPR055263712 (SPR)s10686-024-09936-w-e DE-627 ger DE-627 rakwb eng 520 VZ 39.00 bkl de Kuijper, Kees verfasserin aut Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads 2024 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2024 Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. CubeSat (dpeaa)DE-He213 Gamma-ray astronomy (dpeaa)DE-He213 CZT detector (dpeaa)DE-He213 CZT crystal (dpeaa)DE-He213 Semiconductors (dpeaa)DE-He213 Astrophotonics (dpeaa)DE-He213 Diwan, Rishank verfasserin aut Pal, Partha Sarathi verfasserin aut Ritter, Andreas verfasserin aut Parkinson, Pablo M. Saz verfasserin aut Kong, Andy C. T. verfasserin aut Parker, Quentin A. verfasserin aut Enthalten in Experimental astronomy Springer Netherlands, 1989 57(2024), 2 vom: 23. März (DE-627)312841116 (DE-600)2012330-9 1572-9508 nnns volume:57 year:2024 number:2 day:23 month:03 https://dx.doi.org/10.1007/s10686-024-09936-w X:SPRINGER Resolving-System kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 39.00 VZ AR 57 2024 2 23 03 |
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10.1007/s10686-024-09936-w doi (DE-627)SPR055263712 (SPR)s10686-024-09936-w-e DE-627 ger DE-627 rakwb eng 520 VZ 39.00 bkl de Kuijper, Kees verfasserin aut Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads 2024 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2024 Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. CubeSat (dpeaa)DE-He213 Gamma-ray astronomy (dpeaa)DE-He213 CZT detector (dpeaa)DE-He213 CZT crystal (dpeaa)DE-He213 Semiconductors (dpeaa)DE-He213 Astrophotonics (dpeaa)DE-He213 Diwan, Rishank verfasserin aut Pal, Partha Sarathi verfasserin aut Ritter, Andreas verfasserin aut Parkinson, Pablo M. Saz verfasserin aut Kong, Andy C. T. verfasserin aut Parker, Quentin A. verfasserin aut Enthalten in Experimental astronomy Springer Netherlands, 1989 57(2024), 2 vom: 23. März (DE-627)312841116 (DE-600)2012330-9 1572-9508 nnns volume:57 year:2024 number:2 day:23 month:03 https://dx.doi.org/10.1007/s10686-024-09936-w X:SPRINGER Resolving-System kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 39.00 VZ AR 57 2024 2 23 03 |
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10.1007/s10686-024-09936-w doi (DE-627)SPR055263712 (SPR)s10686-024-09936-w-e DE-627 ger DE-627 rakwb eng 520 VZ 39.00 bkl de Kuijper, Kees verfasserin aut Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads 2024 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2024 Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. CubeSat (dpeaa)DE-He213 Gamma-ray astronomy (dpeaa)DE-He213 CZT detector (dpeaa)DE-He213 CZT crystal (dpeaa)DE-He213 Semiconductors (dpeaa)DE-He213 Astrophotonics (dpeaa)DE-He213 Diwan, Rishank verfasserin aut Pal, Partha Sarathi verfasserin aut Ritter, Andreas verfasserin aut Parkinson, Pablo M. Saz verfasserin aut Kong, Andy C. T. verfasserin aut Parker, Quentin A. verfasserin aut Enthalten in Experimental astronomy Springer Netherlands, 1989 57(2024), 2 vom: 23. März (DE-627)312841116 (DE-600)2012330-9 1572-9508 nnns volume:57 year:2024 number:2 day:23 month:03 https://dx.doi.org/10.1007/s10686-024-09936-w X:SPRINGER Resolving-System kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 39.00 VZ AR 57 2024 2 23 03 |
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10.1007/s10686-024-09936-w doi (DE-627)SPR055263712 (SPR)s10686-024-09936-w-e DE-627 ger DE-627 rakwb eng 520 VZ 39.00 bkl de Kuijper, Kees verfasserin aut Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads 2024 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2024 Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. CubeSat (dpeaa)DE-He213 Gamma-ray astronomy (dpeaa)DE-He213 CZT detector (dpeaa)DE-He213 CZT crystal (dpeaa)DE-He213 Semiconductors (dpeaa)DE-He213 Astrophotonics (dpeaa)DE-He213 Diwan, Rishank verfasserin aut Pal, Partha Sarathi verfasserin aut Ritter, Andreas verfasserin aut Parkinson, Pablo M. Saz verfasserin aut Kong, Andy C. T. verfasserin aut Parker, Quentin A. verfasserin aut Enthalten in Experimental astronomy Springer Netherlands, 1989 57(2024), 2 vom: 23. März (DE-627)312841116 (DE-600)2012330-9 1572-9508 nnns volume:57 year:2024 number:2 day:23 month:03 https://dx.doi.org/10.1007/s10686-024-09936-w X:SPRINGER Resolving-System kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 39.00 VZ AR 57 2024 2 23 03 |
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10.1007/s10686-024-09936-w doi (DE-627)SPR055263712 (SPR)s10686-024-09936-w-e DE-627 ger DE-627 rakwb eng 520 VZ 39.00 bkl de Kuijper, Kees verfasserin aut Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads 2024 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2024 Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. CubeSat (dpeaa)DE-He213 Gamma-ray astronomy (dpeaa)DE-He213 CZT detector (dpeaa)DE-He213 CZT crystal (dpeaa)DE-He213 Semiconductors (dpeaa)DE-He213 Astrophotonics (dpeaa)DE-He213 Diwan, Rishank verfasserin aut Pal, Partha Sarathi verfasserin aut Ritter, Andreas verfasserin aut Parkinson, Pablo M. Saz verfasserin aut Kong, Andy C. T. verfasserin aut Parker, Quentin A. verfasserin aut Enthalten in Experimental astronomy Springer Netherlands, 1989 57(2024), 2 vom: 23. März (DE-627)312841116 (DE-600)2012330-9 1572-9508 nnns volume:57 year:2024 number:2 day:23 month:03 https://dx.doi.org/10.1007/s10686-024-09936-w X:SPRINGER Resolving-System kostenfrei Volltext SYSFLAG_0 GBV_SPRINGER SSG-OPC-AST GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_120 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 39.00 VZ AR 57 2024 2 23 03 |
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de Kuijper, Kees @@aut@@ Diwan, Rishank @@aut@@ Pal, Partha Sarathi @@aut@@ Ritter, Andreas @@aut@@ Parkinson, Pablo M. Saz @@aut@@ Kong, Andy C. T. @@aut@@ Parker, Quentin A. @@aut@@ |
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However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. 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de Kuijper, Kees |
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de Kuijper, Kees ddc 520 bkl 39.00 misc CubeSat misc Gamma-ray astronomy misc CZT detector misc CZT crystal misc Semiconductors misc Astrophotonics Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads |
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520 VZ 39.00 bkl Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads CubeSat (dpeaa)DE-He213 Gamma-ray astronomy (dpeaa)DE-He213 CZT detector (dpeaa)DE-He213 CZT crystal (dpeaa)DE-He213 Semiconductors (dpeaa)DE-He213 Astrophotonics (dpeaa)DE-He213 |
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evaluation of the performance of a cdznte-based soft $$\gamma $$-ray detector for cubesat payloads |
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Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads |
abstract |
Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. © The Author(s) 2024 |
abstractGer |
Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. © The Author(s) 2024 |
abstract_unstemmed |
Abstract The low-energy $$\varvec{\gamma }$$-ray (0.1-30 MeV) sky has been relatively unexplored since the decommissioning of the COMPTEL instrument on the Compton Gamma-Ray Observatory (CGRO) satellite in 2000. However, the study of this part of the energy spectrum (the “MeV gap”) is crucial for addressing numerous unresolved questions in high-energy and multi-messenger astrophysics. Although several large MeV $$\varvec{\gamma }$$-ray missions like AMEGO and e-ASTROGAM are being proposed, they are predominantly in the developmental phase, with launches not anticipated until the next decade at the earliest. In recent times, there has been a surge in proposed CubeSat missions as cost-effective and rapidly implementable “pathfinder” alternatives. A MeV CubeSat dedicated to $$\varvec{\gamma }$$-ray astronomy has the potential to serve as a demonstrator for future, larger-scale MeV payloads. This paper presents a $$\varvec{\gamma }$$-ray payload design featuring a CdZnTe crystal calorimeter module developed by IDEAS. We report the detailed results of simulations to assess the performance of this proposed payload and compare it with those of previous $$\varvec{\gamma }$$-ray instruments. © The Author(s) 2024 |
collection_details |
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container_issue |
2 |
title_short |
Evaluation of the performance of a CdZnTe-based soft $$\gamma $$-ray detector for CubeSat payloads |
url |
https://dx.doi.org/10.1007/s10686-024-09936-w |
remote_bool |
true |
author2 |
Diwan, Rishank Pal, Partha Sarathi Ritter, Andreas Parkinson, Pablo M. Saz Kong, Andy C. T. Parker, Quentin A. |
author2Str |
Diwan, Rishank Pal, Partha Sarathi Ritter, Andreas Parkinson, Pablo M. Saz Kong, Andy C. T. Parker, Quentin A. |
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doi_str |
10.1007/s10686-024-09936-w |
up_date |
2024-07-03T14:27:08.230Z |
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|
score |
7.400199 |