Solar Power Generation System for the Canadian Space Agency STRATOS Program
This paper discusses the design and application of solar photovoltaics (PV) under aerospace conditions. The application of solar PV that is addressed is the Power Distribution Unit (PDU) for the Canadian Space Agency’s (CSA) stratospheric balloon (STRATOS) program. The PDU utilizes four 1 kWh Batter...
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2021-01-01
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Online Access: | https://www.e3s-conferences.org/articles/e3sconf/pdf/2021/15/e3sconf_icren2021_00006.pdf |
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doaj-38f6e720d12d48d8a33aed7dfc9396ab2021-02-18T10:43:51ZengEDP SciencesE3S Web of Conferences2267-12422021-01-012390000610.1051/e3sconf/202123900006e3sconf_icren2021_00006Solar Power Generation System for the Canadian Space Agency STRATOS ProgramDoulfikar Amine0Cabales Ian1Hossan Akash2Bloemink Jeff3Taheri Pooya4British Columbia Institute of Technology, ECET DepartmentBritish Columbia Institute of Technology, ECET DepartmentBritish Columbia Institute of Technology, ECET DepartmentBritish Columbia Institute of Technology, ECET DepartmentBritish Columbia Institute of Technology, ECET DepartmentThis paper discusses the design and application of solar photovoltaics (PV) under aerospace conditions. The application of solar PV that is addressed is the Power Distribution Unit (PDU) for the Canadian Space Agency’s (CSA) stratospheric balloon (STRATOS) program. The PDU utilizes four 1 kWh Battery Unit (BUs) that have been sized with volume and weight restrictions in mind. Without the capacity to provide enough energy to support multi-day missions, they are thus supplemented by the solar power generation subsystem presented in this paper. The power generation sub-system includes a bespoke solar panel design and a centralized Maximum Power Point Tracking (MPPT) power conversion unit to maximize the power output of solar panels. The centralized unit can accommodate up to eight solar panels, each consisting of nine individual C60 SunPower solar cells. The centralized MPPT unit consists of two MPPT controllers, each controller supporting up to four solar panels. The MPPT unit is modular and can be easily integrated to the CSA’s existing intelligent Battery Management System (BMS).https://www.e3s-conferences.org/articles/e3sconf/pdf/2021/15/e3sconf_icren2021_00006.pdfmppt controllersolar power generationstratoscanadian space agencystratospheric balloonaerospace |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Doulfikar Amine Cabales Ian Hossan Akash Bloemink Jeff Taheri Pooya |
spellingShingle |
Doulfikar Amine Cabales Ian Hossan Akash Bloemink Jeff Taheri Pooya Solar Power Generation System for the Canadian Space Agency STRATOS Program E3S Web of Conferences mppt controller solar power generation stratos canadian space agency stratospheric balloon aerospace |
author_facet |
Doulfikar Amine Cabales Ian Hossan Akash Bloemink Jeff Taheri Pooya |
author_sort |
Doulfikar Amine |
title |
Solar Power Generation System for the Canadian Space Agency STRATOS Program |
title_short |
Solar Power Generation System for the Canadian Space Agency STRATOS Program |
title_full |
Solar Power Generation System for the Canadian Space Agency STRATOS Program |
title_fullStr |
Solar Power Generation System for the Canadian Space Agency STRATOS Program |
title_full_unstemmed |
Solar Power Generation System for the Canadian Space Agency STRATOS Program |
title_sort |
solar power generation system for the canadian space agency stratos program |
publisher |
EDP Sciences |
series |
E3S Web of Conferences |
issn |
2267-1242 |
publishDate |
2021-01-01 |
description |
This paper discusses the design and application of solar photovoltaics (PV) under aerospace conditions. The application of solar PV that is addressed is the Power Distribution Unit (PDU) for the Canadian Space Agency’s (CSA) stratospheric balloon (STRATOS) program. The PDU utilizes four 1 kWh Battery Unit (BUs) that have been sized with volume and weight restrictions in mind. Without the capacity to provide enough energy to support multi-day missions, they are thus supplemented by the solar power generation subsystem presented in this paper. The power generation sub-system includes a bespoke solar panel design and a centralized Maximum Power Point Tracking (MPPT) power conversion unit to maximize the power output of solar panels. The centralized unit can accommodate up to eight solar panels, each consisting of nine individual C60 SunPower solar cells. The centralized MPPT unit consists of two MPPT controllers, each controller supporting up to four solar panels. The MPPT unit is modular and can be easily integrated to the CSA’s existing intelligent Battery Management System (BMS). |
topic |
mppt controller solar power generation stratos canadian space agency stratospheric balloon aerospace |
url |
https://www.e3s-conferences.org/articles/e3sconf/pdf/2021/15/e3sconf_icren2021_00006.pdf |
work_keys_str_mv |
AT doulfikaramine solarpowergenerationsystemforthecanadianspaceagencystratosprogram AT cabalesian solarpowergenerationsystemforthecanadianspaceagencystratosprogram AT hossanakash solarpowergenerationsystemforthecanadianspaceagencystratosprogram AT bloeminkjeff solarpowergenerationsystemforthecanadianspaceagencystratosprogram AT taheripooya solarpowergenerationsystemforthecanadianspaceagencystratosprogram |
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