摘要
针对火星环绕探测任务特点,从空间环境,飞行程序、轨道与姿态,负载需求,电源系统选型,能源自主管理,轻小型化设计6个方面对电源系统设计进行了分析;提出了一种适用于火星环绕探测器的高比能量、高比功率、高自主管理能力的电源系统设计分析方法,可为火星环绕探测器电源系统优化设计提供依据,也可为其他深空探测器电源系统设计提供一定的借鉴与参考。
According to the specific characteristics of Mars orbiting exploration, the factors influencing the power system design are analyzed, such as space environment, designated flight schedule, orbit and attitude, load power requirement, power system topology selection, power system self-management,light weight and scale design. A method is provided for high specific energy, high specific power and high autonomous management power system design and analysis for Mars orbiting probe. The method can not only be a basis for the optimization design of Mars orbiting probe power system,but also be used as a reference for the power system design of other deep space probes.
出处
《航天器工程》
2013年第1期60-64,共5页
Spacecraft Engineering
