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Titlebook: Spacecraft Power System Technologies; Qi Chen,Zhigang Liu,Liying Zhu Book 2020 Beijing Institute of Technology Press and Springer Nature S

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31#
發(fā)表于 2025-3-26 23:49:19 | 只看該作者
Introduction, physical or chemical changes, so as to store, regulate, and convert the electrical energy as required, and to supply and distribute electrical power to individual spacecraft equipment in various phases, including the launching phase, the orbit transferring phase, and the on-orbit lifetime.
32#
發(fā)表于 2025-3-27 02:28:10 | 只看該作者
Design of Primary Power Subsystem, satellite mission, orbital lighting conditions, satellite attitude and life, radiation damage, power component performance degradation, and external characteristics of solar cells and battery, then make a choice, and finally give the optimal design results of system performance, mass, size, reliability, and cost.
33#
發(fā)表于 2025-3-27 08:14:44 | 只看該作者
Design of System Circuit Subsystem (SCS),ation topology of spacecraft load distribution, EED initiation, secondary power conversion, signal rate power, and information topology, as well as the interfaces with launch vehicle, ground test system, and other space subsystems.
34#
發(fā)表于 2025-3-27 11:49:49 | 只看該作者
Reliability and Safety Design for Power System,cts with high-level maturity, and the productized and modularization products should be applied in a maximum manner. The new technologies without flight experience should be verified by adequate ground testing.
35#
發(fā)表于 2025-3-27 14:56:56 | 只看該作者
36#
發(fā)表于 2025-3-27 17:59:16 | 只看該作者
37#
發(fā)表于 2025-3-28 00:45:53 | 只看該作者
Further Space Task demands and Power System Development Trends,d high efficiency. The system circuit system is gradually evolving from centralized power supply to distributed power supply, intelligent power distribution management, and fault diagnosis and isolation.
38#
發(fā)表于 2025-3-28 03:51:06 | 只看該作者
Design Example of Power System,This chapter will briefly introduce the power system design of a geostationary orbit satellite (GEO satellite) developed by the China Academy of Space Technology. The total weight of this satellite is 3700?kg and its designed lifetime is 15?years.
39#
發(fā)表于 2025-3-28 10:17:55 | 只看該作者
Qi Chen,Zhigang Liu,Liying ZhuProvides readers with detailed concepts and design theories for space power systems.Presents the procedures and design methods for power system reliability and security, risk analysis and control, tes
40#
發(fā)表于 2025-3-28 14:25:33 | 只看該作者
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