The electromagnetic environment of spacecraft is analyzed, and several EMC problems in spacecraft system design are pointed out.
分析了空间飞行器所处的电磁环境，指出总体设计中的若干电磁兼容性问题；
The SOC design and implementation of the spacecraft system bus was studied, for example of the 1553b bus controller.
以1553 B总线控制器为例，采用SOC设计方法，研究了航天器系统总线的设计和实现。
The companies will provide data related to the development of their Crew Transportation System (CTS) design, including a spacecraft, launch vehicle, ground and mission operations and recovery.
这些公司将提供开发他们乘员运输系统(CTS)设计的有关数据，航天器，运载火箭，地面和任务运转以及回收。
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