2019 European Space Power Conference (ESPC)最新文献

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High-Efficiency Low Voltage/High Current Power Supplies for High Performance Digital Equipment by using GaN FET Technology 基于GaN场效应管技术的高性能数字设备的高效低压/大电流电源
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8931977
Franz Stoegerer, T. Panhofer
{"title":"High-Efficiency Low Voltage/High Current Power Supplies for High Performance Digital Equipment by using GaN FET Technology","authors":"Franz Stoegerer, T. Panhofer","doi":"10.1109/ESPC.2019.8931977","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8931977","url":null,"abstract":"High performance processing boards using ASICs and reconfigurable FPGAs require particular power supplies with voltages below 1 V and current capabilities up to 50 A. High efficiency is mandatory for low power consumption and thermal reasons and is considered as most important goal for the DCDC converter. Off-the-shelf radiation hardened point-of-load (POL) converters are not optimized for such an application. Most devices are limited to approximately 10 A and show maximum efficiency at approximately half load current. Only a few parts offer the possibility for parallel operation to increase the current capability. Apart from the non-isolating POL converters also high-current supplies based on an isolated converter topology with good efficiency are available on the market. The efficiency of both concepts relies on high-performance/low-on-resistance FETs, and GaN technology seems to be a very attractive solution. This paper evaluates discrete designs of a non-isolating POL converter and an isolating converter based on GaN FETs regarding their suitability for low voltage/high current applications. Beside of theoretical investigations, experimental results gained from laboratory prototypes are presented.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"8 1","pages":"1-7"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"81591992","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Identification of COTS Cells to Meet Space Market Segment Requirements 识别COTS单元以满足空间细分市场的要求
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932047
Alex Clarke, R. Buckle
{"title":"Identification of COTS Cells to Meet Space Market Segment Requirements","authors":"Alex Clarke, R. Buckle","doi":"10.1109/ESPC.2019.8932047","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932047","url":null,"abstract":"The Space market can be segmented according to the requirements applicable to specific applications. For example, LEO missions are characterised by the requirement for a high number of cycles at low DoD, whereas GEO missions require the battery to be cycled at high DoD. These different drivers mean that one cell type may not be optimal for all types of mission, in terms of minimising the mass and volume of the battery. This paper discusses ABSL's expanded cell portfolio, and how the requirements of the various applications are met by the identified cell types","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"397 1","pages":"1-4"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"85023699","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
Regolith Packed Bed Thermal Energy Storage for Lunar Night Survival 月球夜间生存的风化层填充床热能储存
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932053
S. Fereres, Sergio Escario, C. Prieto, S. de La Rosa
{"title":"Regolith Packed Bed Thermal Energy Storage for Lunar Night Survival","authors":"S. Fereres, Sergio Escario, C. Prieto, S. de La Rosa","doi":"10.1109/ESPC.2019.8932053","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932053","url":null,"abstract":"In-Situ Resource Utilization (ISRU) technologies for future deep-space exploration is a current hot topic considering planned lunar missions for the coming years. Energy generation and storage using regolith can be useful not only for future lunar human outposts but also to assist lunar mining or construction activities during the lunar night. Here we explore the design of a packed bed Thermal Energy Storage (TES) system using regolith as the storage media through a numerical model. System requirements are analyzed depending on landing sites and mission needs. Different heat transfer fluids (HTF) are evaluated for the TES charge/discharge, using media available from other complementary ISRU processes (i.e. oxygen/water production from lunar regolith) or gases indispensable for life support systems. Raw regolith of varied composition, several Earth materials and processed/reduced regolith are compared, and different TES integration options are discussed.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"23 1","pages":"1-7"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"83756908","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Transformer optimization for 3D PLUS Universal RCN Front End converter 3D PLUS通用RCN前端转换器的变压器优化
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932006
Cédric Colonna, P. Dubus, D. Labrousse
{"title":"Transformer optimization for 3D PLUS Universal RCN Front End converter","authors":"Cédric Colonna, P. Dubus, D. Labrousse","doi":"10.1109/ESPC.2019.8932006","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932006","url":null,"abstract":"To be compatible with all the existing spacecraft, 3D PLUS is developing a Front end power converter, which works from DC18V to DC110V for the input voltage, from DC3V for the output voltage and from 0W to 50W for the output power. The transformer design is critical because it should not penalize the operation of the converter in a reduced size. This document will first define the topology of the transformer. It will then discuss the different loss models chosen to optimize the sizing. An optimization combining multi-physical finite element computation and a multi-objective genetic optimization algorithm will then be introduced. After a comparison between different materials int term of occupied surface with fixed maximum heating, we will conclude this study by presenting the realization and implementation of our transformer.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"26 1","pages":"1-8"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"84339779","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Accurate Solar Cell Measurements at Low Temperatures using a Cryostat 使用低温恒温器在低温下精确测量太阳能电池
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932073
G. Siefer, E. Fehrenbacher, M. Schachtner, A. Wekkeli
{"title":"Accurate Solar Cell Measurements at Low Temperatures using a Cryostat","authors":"G. Siefer, E. Fehrenbacher, M. Schachtner, A. Wekkeli","doi":"10.1109/ESPC.2019.8932073","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932073","url":null,"abstract":"Calibrated measurements of solar cells at low temperatures are of specific interest for various space missions, for example to Mars and Jupiter. In the past 15 years, several hundred triple-junction and component solar cells have been measured at the solar cell calibration laboratory at Fraunhofer ISE (CalLab PV Cells), mainly in the frame of the European Space Agency (ESA) programs ExoMars and JUICE. To allow for measurements at temperatures as low as 123 K a specially developed cryostat setup is being used. This paper summarizes the main challenges and findings in respect to measurement procedures and calibration of solar cells under low temperature conditions, including the mounting of the solar cells, control of the correct solar cell temperature, and definition of the correct illumination spectrum and intensity.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"59 1","pages":"1-4"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"80503270","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Power Assessment Indices of Solar Arrays under MPPT and DET methods for Spacecraft 航天器太阳能电池阵在MPPT和DET方法下的功率评估指标
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932076
Zhang Xuan, Kang Qing, Y. Wentao, Xing Jie, Li Feng, You Xiangan
{"title":"Power Assessment Indices of Solar Arrays under MPPT and DET methods for Spacecraft","authors":"Zhang Xuan, Kang Qing, Y. Wentao, Xing Jie, Li Feng, You Xiangan","doi":"10.1109/ESPC.2019.8932076","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932076","url":null,"abstract":"In order to measure power utilization ratio of solar arrays under Maximum Power Point Tracking(MPPT) and three different Direct Energy Transfer(DET) solutions quantitatively, this paper defines two power indices, energy loss percentage(ELP) and energy excess percentage(EEP), as the basis of satellite power system design. This paper also gives the calculation of these two indices based on the feature of joint-operation of PV and batteries, the control efficiency and the design margin. On the basis of ELP and EPP, two applicable cases of MPPT and DET architecture are analyzed. Computation results show that ELP of MPPT is better while EEP of DET is more competitive.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"1 1","pages":"1-4"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"86524994","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
Batteries for Satellites Constellation, using Lean Manufacturing for Space Industry 卫星星座电池,航天工业精益制造
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932064
Laurence Perino-Gallice, O. Masson, M. Bel, F. Fusalba
{"title":"Batteries for Satellites Constellation, using Lean Manufacturing for Space Industry","authors":"Laurence Perino-Gallice, O. Masson, M. Bel, F. Fusalba","doi":"10.1109/ESPC.2019.8932064","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932064","url":null,"abstract":"“The space revolution is being led by more than Musk and Bezos”, Backstage, aerospace leaders and their suppliers already work on design to cost engineering using automatized processes and working to qualify COTS within Lean manufacturing method. In 2014, CEA did propose the use of Commercial Off The Shelf (COTS) 18650 Li-ion cells to manufacture competitive aerospace batteries (without modifications for space use managing space qualification at system level) and in 2015 the use of Lean 6 sigma manufacturing approach based on its automotive/terrestrial industry experience to respond new space requirements. Our development phase continuously challenged Design to Cost & Design to Industrialization (Series Manufacturing). As a result, the battery product integrates COTS 18650 Li-ion cells and hardware. Its price breakdown targeted for competitive product industrialization is reached under space qualification. Manufactured within an Iso 8 clean room for space use, a Manufacturing Execution System (MES) manages its industrial quality. Our tool, sized for fast prototyping and transfer towards industry, eases demonstration to industrialization maturity assessments (time & cost to market). We built a battery assembly line from scratch to operation in 8 months and, following an ISO10005 completed with EN9100 quality plan, we space qualified its processes in 15 months, product ready for launch within 24 months. First flight models integrate OneWeb constellation satellites set for launch Feb. 2019. By now, recurring products for space applications are continuously running through standards processes. CEA demonstrated its industry-oriented results with a highly agile battery assembly line transfer, proving shorten assembly times with means to analyze factory performance and process improvements under space standards. Manufacturing data under the production method necessary to manufacture high-performance batteries to power satellites constellation are discussed in this paper. This approach is applicable for other space equipment.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"7 1","pages":"1-6"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"75116045","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
Revised stability criteria for cascaded DC-DC converters in space applications 修订的空间应用级联DC-DC变换器稳定性标准
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932078
M. Triggianese, H. Carbonnier, F. Tonicello
{"title":"Revised stability criteria for cascaded DC-DC converters in space applications","authors":"M. Triggianese, H. Carbonnier, F. Tonicello","doi":"10.1109/ESPC.2019.8932078","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932078","url":null,"abstract":"The Middlebrook's criteria is used in the ECSS-E-ST −20C (European Cooperation for Space Standardization - Electrical and Electronic) to guarantee the stability of cascaded power systems. It is worth noticing that the non-compliance to Middlebrook's criterion does not represent a necessary condition for stability, therefore when not satisfied, additional analysis might be necessary to check the stability margins. It is however a very conservative approach. Other less conservative methods have been proposed for the interconnection of feedback controlled DC/DC converters. Among others, a revised criterion is considered in this paper and different study-cases are analyzed to demonstrate the typical situations that a power engineer is facing with cascaded DC-DC power supplies.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"157 1","pages":"1-6"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"73921010","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
An optimization strategy for battery charging in small satellites 小卫星电池充电优化策略研究
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932032
Elisa Mostacciuolo, F. Vasca, Silvio Baccari, L. Iannelli, Salvatore Sagnelli, Raffaele Luisi, V. Stanzione
{"title":"An optimization strategy for battery charging in small satellites","authors":"Elisa Mostacciuolo, F. Vasca, Silvio Baccari, L. Iannelli, Salvatore Sagnelli, Raffaele Luisi, V. Stanzione","doi":"10.1109/ESPC.2019.8932032","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932032","url":null,"abstract":"A model-based optimization of the charging process of batteries in small satellites is proposed. The battery is considered as part of an electrical power system with a peak power tracker architecture and an unregulated bus. Real data are used to determine the parameters of the dynamic model of the system. The battery charging optimization is obtained through the minimization of a cost function which weights charging time, energy losses and temperature variations by taking into account also the dynamic model. Simulation results show the validity of the proposed solution in terms of performance and computational effort for different missions power load, irradiance and temperature operating conditions.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"41 1","pages":"1-8"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"88223312","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 2
MP XLR battery range for constellation MP XLR电池范围星座
2019 European Space Power Conference (ESPC) Pub Date : 2019-09-01 DOI: 10.1109/ESPC.2019.8932000
A. Vanessa, Clemente Jacky, Jérémy Hyvert, Godon Aurelie, P. J. Paul, Remy Stéphane, Borthomieu Yannick
{"title":"MP XLR battery range for constellation","authors":"A. Vanessa, Clemente Jacky, Jérémy Hyvert, Godon Aurelie, P. J. Paul, Remy Stéphane, Borthomieu Yannick","doi":"10.1109/ESPC.2019.8932000","DOIUrl":"https://doi.org/10.1109/ESPC.2019.8932000","url":null,"abstract":"There are two major challenges for Saft to develop a battery design for LEO satellite constellation which is out of the ordinary: lean production as well as a disruptive cost approach. Those main ideas will be the primordial drivers from the beginning to the end of the project. To reach the target, Saft is looking for answers to: how to build more efficiently and quickly, how to pack more simply and how to be able to run in parallel huge number to blocks? Saft core business is in energy storage system. Hence, it will use its in-house COTS cell called MP xlr for the fabrication of batteries for constellation purposes. MP xlr cells has demonstrated 1800 cycles @ 100% DOD while retaining 70% of its initial capacity. The performance of the MP xlr cell evaluated at 20% DOD and 30% DOD LEO cycling also shows a very good trend in EODV similarly to VES16 cell a space dedicated cell. Moreover, MP xlr cell exhibits stable internal resistance over cycle life which gives a significant advantage at battery level from the voltage stability to heat generation that is constant over the life.","PeriodicalId":6734,"journal":{"name":"2019 European Space Power Conference (ESPC)","volume":"13 1","pages":"1-8"},"PeriodicalIF":0.0,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"90773227","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 1
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