《Spacecraft power system technologies》是2020年9月北京理工大學出版社出版的圖書，作者是陳琪。
基本介紹
- 中文名：Spacecraft power system technologies
- 作者：陳琪
- 出版社：北京理工大學出版社
- ISBN：9787568290630
內容簡介,圖書目錄,
內容簡介
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.
圖書目錄
1 Introduction
1．1 Definitions and Function□<□r>1．□ Classification and Composition
1．2Classification
1.2.1Composition
1.2.2Primary Power Subsystem
1．3．1 Power Generation Technologie□<□r>1．3．□ 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 Phase□<□r>1．5．□ Development Proces□<□r>1．6 Power System Evaluation
1．7 Development of Spacecraft Power System in China
1．7．1 Development of Spacecraft Power System Technology
1．7．2Development of Spacecraft Power Distribution
Technology and SCS Technology
Reference□<□r>
Design of Primary Power Subsystem
1 Design Basis and Constraint□<□r>□．1．1 Space Environment and Its Effect□<□r>□．1．□ Flight Mission
1．3 Mutual Constraints in the Design of Spacecraft Power System
1．4 Flight Procedure
1．5 Lighting Condition□<□r>□．1．6 Payload Configuration and Load Characteristic□<□r>□．□ Power System Topology
1 Bus Voltage
Bus Configuration
3 Power Regulation of Solar Array□<□r>□．□．4 Energy Transfer Method
5 Bus Voltage Regulation Method□<□r>□．□．6 Installation of Solar Array
3 Design and Calculation of Power System
3．1 Solar Array
3．2 Battery Pack
3．3 Power Control Unit （PCU）
3．4 Energy Balance Analysi□<□r>Reference□<□r>
3 Design of System Circuit Subsystem （SCS）
3．1 General
3．2 Working Environment and Constraint□<□r>3．□．1 Electromagnetic Environment
3．3 Mechanical Environment
3．4 Thermal Environment
3．4.1 Space Environment
3．5 Other Environment□<□r>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． Design of Spacecraft Grounding and Lapping
3．4．3 Design Examples of Spacecraft Grounding and Lapping
3．5 Design of System Circuit Interface□<□r>3．5．1 General
3．5． Design of Iter face Between Satellite （Spacecraft）and Rocket
3．5．3 Design of Interface Between Satellite （Spacecraft）and Ground
3．5．4 Design of Other Key Interface□<□r>3．6 Design of System Circuit
3．6．1 Power Distribution Unit （PDU）
……
4 Design Example of Power System
5 Reliability and Safety Design for Power System
6 Analysis and Control of Technical Risks in Power System
7 Power System Testing and Environment Experiment□<□r>8 Autonomous Management of Power System
9 Further Space Task demands and Power System Development
Trends
