A Design of Solar Proton Telescope for Next Generation Small Satellite

The solar proton telescope (SPT) is considered as one of the scientific instruments to be installed in instruments for the study of space storm (ISSS) which is determined for next generation small satellite-1 (NEXTSat-1). The SPT is the instrument that acquires the information on energetic particles...

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Main Authors: Jongdae Sohn, Suyeon Oh, Yu Yi, Kyoung-Wook Min, Dae-Young Lee, Jongho Seon
Format: Article
Language:English
Published: The Korean Space Science Society 2012-12-01
Series:Journal of Astronomy and Space Sciences
Subjects:
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2012/v29n4/OJOOBS_2012_v29n4_343.pdf
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author Jongdae Sohn
Suyeon Oh
Yu Yi
Kyoung-Wook Min
Dae-Young Lee
Jongho Seon
author_facet Jongdae Sohn
Suyeon Oh
Yu Yi
Kyoung-Wook Min
Dae-Young Lee
Jongho Seon
author_sort Jongdae Sohn
collection DOAJ
description The solar proton telescope (SPT) is considered as one of the scientific instruments to be installed in instruments for the study of space storm (ISSS) which is determined for next generation small satellite-1 (NEXTSat-1). The SPT is the instrument that acquires the information on energetic particles, especially the energy and flux of proton, according to the solar activity in the space radiation environment. We performed the simulation to determine the specification of the SPT using geometry and tracking 4 (GEANT4). The simulation was performed in the range of 0.6-1,000 MeV considering that the proton, which is to be detected, corresponds to the high energy region according to the solar activity in the space radiation environment. By using aluminum as a blocking material and adjusting the energy detection range, we determined total 7 channels (0.6~5, 5~10, 10~20, 20~35, 35~52, 52~72, and >72 MeV) for the energy range of SPT. In the SPT, the proton energy was distinguished using linear energy transfer to compare with or discriminate from relativistic electron for the channels P1-P3 which are the range of less than 20 MeV, and above those channels, the energy was determined on the basis of whether silicon semiconductor detector (SSD) signal can pass or not. To determine the optimal channel, we performed the conceptual design of payload which uses the SSD. The designed SPT will improve the understanding on the capture and decline of solar energetic particles at the radiation belt by measuring the energetic proton.
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spelling doaj.art-30796270762844ecbe0546cbadec55cc2024-01-02T02:51:17ZengThe Korean Space Science SocietyJournal of Astronomy and Space Sciences2093-55872093-14092012-12-0129434334910.5140/JASS.2012.29.4.343A Design of Solar Proton Telescope for Next Generation Small SatelliteJongdae Sohn0Suyeon Oh1Yu Yi2Kyoung-Wook Min3Dae-Young Lee4Jongho Seon5Department of Astronomy and Space Science, Chungnam National University, Daejeon 305-764, KoreaDepartment of Astronomy and Space Science, Chungnam National University, Daejeon 305-764, KoreaDepartment of Astronomy and Space Science, Chungnam National University, Daejeon 305-764, KoreaDepartment of Physics, Korea Advanced Institute of Science and Technology, Daejeon 305-701, KoreaDepartment of Astronomy and Space Science, Chungbuk National University, Cheongju 361-763, KoreaSchool of Space Research, Kyung Hee University, Yongin 446-701, KoreaThe solar proton telescope (SPT) is considered as one of the scientific instruments to be installed in instruments for the study of space storm (ISSS) which is determined for next generation small satellite-1 (NEXTSat-1). The SPT is the instrument that acquires the information on energetic particles, especially the energy and flux of proton, according to the solar activity in the space radiation environment. We performed the simulation to determine the specification of the SPT using geometry and tracking 4 (GEANT4). The simulation was performed in the range of 0.6-1,000 MeV considering that the proton, which is to be detected, corresponds to the high energy region according to the solar activity in the space radiation environment. By using aluminum as a blocking material and adjusting the energy detection range, we determined total 7 channels (0.6~5, 5~10, 10~20, 20~35, 35~52, 52~72, and >72 MeV) for the energy range of SPT. In the SPT, the proton energy was distinguished using linear energy transfer to compare with or discriminate from relativistic electron for the channels P1-P3 which are the range of less than 20 MeV, and above those channels, the energy was determined on the basis of whether silicon semiconductor detector (SSD) signal can pass or not. To determine the optimal channel, we performed the conceptual design of payload which uses the SSD. The designed SPT will improve the understanding on the capture and decline of solar energetic particles at the radiation belt by measuring the energetic proton.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2012/v29n4/OJOOBS_2012_v29n4_343.pdfspace stormsolar protoncosmic ray
spellingShingle Jongdae Sohn
Suyeon Oh
Yu Yi
Kyoung-Wook Min
Dae-Young Lee
Jongho Seon
A Design of Solar Proton Telescope for Next Generation Small Satellite
Journal of Astronomy and Space Sciences
space storm
solar proton
cosmic ray
title A Design of Solar Proton Telescope for Next Generation Small Satellite
title_full A Design of Solar Proton Telescope for Next Generation Small Satellite
title_fullStr A Design of Solar Proton Telescope for Next Generation Small Satellite
title_full_unstemmed A Design of Solar Proton Telescope for Next Generation Small Satellite
title_short A Design of Solar Proton Telescope for Next Generation Small Satellite
title_sort design of solar proton telescope for next generation small satellite
topic space storm
solar proton
cosmic ray
url http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2012/v29n4/OJOOBS_2012_v29n4_343.pdf
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