立方体卫星MOVE-II空间太阳能电池在轨验证

2016 IEEE 43rd Photovoltaic Specialists Conference (PVSC) Pub Date : 2016-06-05 DOI:10.1109/PVSC.2016.7750120

M. Rutzinger, L. Krempel, Manuel Salzberger, Mario Buchner, Alexander Hohn, M. Kellner, K. Janzer, C. Zimmermann, M. Langer

{"title":"立方体卫星MOVE-II空间太阳能电池在轨验证","authors":"M. Rutzinger, L. Krempel, Manuel Salzberger, Mario Buchner, Alexander Hohn, M. Kellner, K. Janzer, C. Zimmermann, M. Langer","doi":"10.1109/PVSC.2016.7750120","DOIUrl":null,"url":null,"abstract":"Several promising multi-junction solar cell concepts for space applications are currently under development worldwide. On-Orbit Verification on CubeSats is a cost-efficient method to gain data on critical hardware early in the design validation process. The MOVE-II CubeSat will be used for the verification of novel 4-6 junction solar cells. With a footprint of 10×10 cm2, the payload consists of one full size solar cell (8×4 cm2) and up to 7 positions (each 2×2 cm2) for corresponding isotype solar cells. The measurement electronics is based on commercial off-the-shelf hardware. MOVE-II is planned to launch in early 2018 into a 500-550 km sun-synchronous orbit.","PeriodicalId":6524,"journal":{"name":"2016 IEEE 43rd Photovoltaic Specialists Conference (PVSC)","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"2016-06-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":"{\"title\":\"On-orbit verification of space solar cells on the CubeSat MOVE-II\",\"authors\":\"M. Rutzinger, L. Krempel, Manuel Salzberger, Mario Buchner, Alexander Hohn, M. Kellner, K. Janzer, C. Zimmermann, M. Langer\",\"doi\":\"10.1109/PVSC.2016.7750120\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Several promising multi-junction solar cell concepts for space applications are currently under development worldwide. On-Orbit Verification on CubeSats is a cost-efficient method to gain data on critical hardware early in the design validation process. The MOVE-II CubeSat will be used for the verification of novel 4-6 junction solar cells. With a footprint of 10×10 cm2, the payload consists of one full size solar cell (8×4 cm2) and up to 7 positions (each 2×2 cm2) for corresponding isotype solar cells. The measurement electronics is based on commercial off-the-shelf hardware. MOVE-II is planned to launch in early 2018 into a 500-550 km sun-synchronous orbit.\",\"PeriodicalId\":6524,\"journal\":{\"name\":\"2016 IEEE 43rd Photovoltaic Specialists Conference (PVSC)\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-06-05\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"4\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 IEEE 43rd Photovoltaic Specialists Conference (PVSC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/PVSC.2016.7750120\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 IEEE 43rd Photovoltaic Specialists Conference (PVSC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/PVSC.2016.7750120","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 4

摘要

目前世界范围内正在开发用于空间应用的几个有前途的多结太阳能电池概念。立方体卫星的在轨验证是在设计验证过程的早期获得关键硬件数据的一种经济有效的方法。MOVE-II立方体卫星将用于验证新型4-6结太阳能电池。占地10×10 cm2，有效载荷包括一个全尺寸太阳能电池(8×4 cm2)和多达7个位置(每个2×2 cm2)对应的同型太阳能电池。测量电子是基于商业现成的硬件。MOVE-II计划于2018年初发射到500-550公里的太阳同步轨道。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

On-orbit verification of space solar cells on the CubeSat MOVE-II

Several promising multi-junction solar cell concepts for space applications are currently under development worldwide. On-Orbit Verification on CubeSats is a cost-efficient method to gain data on critical hardware early in the design validation process. The MOVE-II CubeSat will be used for the verification of novel 4-6 junction solar cells. With a footprint of 10×10 cm2, the payload consists of one full size solar cell (8×4 cm2) and up to 7 positions (each 2×2 cm2) for corresponding isotype solar cells. The measurement electronics is based on commercial off-the-shelf hardware. MOVE-II is planned to launch in early 2018 into a 500-550 km sun-synchronous orbit.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

2016 IEEE 43rd Photovoltaic Specialists Conference (PVSC)

自引率

0.00%

发文量