全新正版 航天器电源技术(英文版)(精) 编者:Qi Chen//Zhigang Liu//Xiaofeng Zhang//Liying Zhu|责编:武丽娟 9787568290630 北京理工大学
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作者编者:Qi Chen//Zhigang Liu//Xiaofeng Zhang//Liying Zhu|责编:武丽娟
出版社北京理工大学
ISBN9787568290630
出版时间2020-09
装帧精装
开本其他
定价118元
货号31036162
上书时间2023-06-08
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Thi□ □ook provides an introduction to the main design principles， methods， proceclurcs，and development trends in spacecraft power systems. It is divided into nine chapters，the first of which covers the classification and main components of primary power system design and power distribution system design. In turn， Chapters □ to 4 t'ocus on the spacecraft power system design experience and review the latest typical design cascs concerning spacecraft power systems in China. More specifically， these chapters also introduce readers to the topological structure and key technologies used in spacecraft power systems. Chapters 5 to 7 address power system reliability and safety design，risk analysis and control， and inorbit management in China's spacecraft engineering projects. The book's closing chapters provide essential information on new power systems and technologies， such as space nuclear power， micro- and nano-satellite power systems， and space energy interconnection systems. An outlook on future development trends rounds out the coverage.
作者简介
陈琦，博士，研究员，现任中国空间技术研究院总体部副部长，中国宇航学会空间能源专业委员会委员，国防科工局能源与动力组专家。研究方向为航天器电源系统设计、空间能源技术发展规划。作为主任设计师主持完成以“海洋二号”、资源系列为代表的十余颗卫星电源分系统研制。作为项目负责人主持完成多项民用航天和装备预研项目。2014年获中国航天基金奖，2015年获国防科学技术进步一等奖、中国航天科技集团科学技术进步一等奖，2016年获国家科技进步二等奖。在国内外学术期刊发表论文40余篇，授权专利10余项。
目录
1 Introduction
1.1 Definitions and Functions
1.2 Classification and Composition
1.2.1 Classification
1.2.2 Composition
1.3 Primary Power Subsystem
1.3.1 Power Generation Technologies
1.3.2 Power Storage Technology
1.3.3 Power Control Technology
1.4 System Circuit Subsystem (SCS)
1.4.1 Power Distribution Architecture
1.4.2 Tasks and Configuration of SCS
1.4.3 Overcurrent Protection Technology
1.5 Development Process of Spacecraft Power System
1.5.1 Development Phases
1.5.2 Development Process
1.6 Power System Evaluation
1.7 Development of Spacecraft Power System in China
1.7.1 Development of Spacecraft Power System Technology
1.7.2 Development of Spacecraft Power Distribution Technology and SCS Technology
References
2 Design of Primary Power Subsystem
2.1 Design Basis and Constraints
2.1.1 Space Environment and Its Effects
2.1.2 Flight Mission
2.1.3 Mutual Constraints in the Design of Spacecraft Power System
2.1.4 Flight Procedure
2.1.5 Lighting Conditions
2.1.6 Payload Configuration and Load Characteristics
2.2 Power System Topology
2.2.1 Bus Voltage
2.2.2 Bus Configuration
2.2.3 Power Regulation of Solar Arrays
2.2.4 Energy Transfer Method
2.2.5 Bus Voltage Regulation Methods
2.2.6 Installation of Solar Array
2.3 Design and Calculation of Power System
2.3.1 Solar Array
2.3.2 Battery Pack
2.3.3 Power Control Unit (PCU)
2.3.4 Energy Balance Analysis
References
3 Design of System Circuit Subsystem (SCS)
3.1 General
3.2 Working Environment and Constraints
3.2.1 Electromagnetic Environment
3.2.2 Mechanical Environment
3.2.3 Thermal Environment
3.2.4 Space Environment
3.2.5 Other Environments
3.3 System Design
3.3.1 Design of Load Power Priority
3.3.2 Design of Distribution Bus System
3.3.3 Design of Distribution Bus Control
3.3.4 Bus Protection Design
3.4 Design of Grounding and Lapping
3.4.1 Design of Grounding System
3.4.2 Design of Spacecraft Grounding and Lapping
3.4.3 Design Examples of Spacecraft Grounding and Lapping
3.5 Design of System Circuit Interfaces
3.5.1 General
3.5.2 Design of Interface Between Satellite (Spacecraft) and Rocket
3.5.3 Design of Interface Between Satellite (Spacecraft) and Ground
3.5.4 Design of Other Key Interfaces
3.6 Design of System Circuit
3.6.1 Power Distribution Unit (PDU)
3.6.2 EED Manager
3.6.3 Cable Harness
References
4 Design Example of Power System
4.1 Design Example of Power System of GEO Satellite
4.1.1 Design Conditions
4.1.2 System Design
4.1.3 Solar Array Design
4.1.4 Design of Battery Pack
4.1.5 Design of Power Control Unit (PCU)
4.2 Design Example of Power System of the Satellite
in Sun-Synchronous Orbit
4.2.1 Design Conditions
4.2.2 System Design
4.2.3 Solar Array Design
4.2.4 Design of Battery Packs
4.2.5 PCU Design
4.3 Design Example of Power System of Deep-Space
Exploration
4.3.1 System Design
4.3.2 Design of Solar Array on Lander
4.3.3 Design of Lander Battery Pack
4.3.4 Design of Lander Power Control
4.3.5 Sleep/Wake Design
4.3.6 Technology of Energy Reuse Among Multiple Devices
References
5 Reliability and Safety Design for Power System
5.1 Design Overview
5.2 Prediction and Allocation of Quantitative Reliability
Indicators
5.2.1 Establishment of Reliability Model
5.2.2 Reliability Prediction
5.2.3 Reliability Allocation
5.3 Thermal Design and Mechanical Environment Resistance
Design
5.3.1 Thermal Design
5.3.2 Mechanical Environment Resistance Design
5.4 Design of Derating and Redundancy Margin
5.4.1 Derating Desi
内容摘要
空间电源系统被称为本书是北京理工大学出版社与SpringerNature联合出版图书。
“航天器的心脏”，对保障航天器正常工作起着决定性作用。本书由中国空间技术研究院第一线专家领衔编著，阐述了航天器电源系统的工程设计原理、方法、流程和经验，梳理了国内外典型航天器平台电源系统设计案例，提炼并汇集了各领域航天器电源系统的拓扑结构和关键技术。本书体现了中国科技工作者为推动航天科技事业发展所做出的重要贡献。
重点阐述内容为：①一次电源系统设计和总体电路系统设计；②电源系统可靠性与安全性设计；③电源系统技术风险分析与控制；④电源系统性能测试与环境试验；⑤电源系统在轨运行与管理；⑥电源系统自主管理；⑦通信卫星、导航卫星、遥感卫星、载人航天器、深空探测器电源系统设计；⑧空间任务需求及电源系统与技术发展趋势。
本书是面向空间领域一线科研人员、相关领域研究者、政府决策人员的一部具有指导意义的权威著作。
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