"嫦娥4号"任务将首次实现人类在月球背面软着陆。通过分析任务特点,以多类型有效载荷配置为背景,介绍了以科学目标和探测任务为核心的有效载荷系统设计思路和实现方法。同时针对首次在深空探测领域搭载国际合作有效载荷项目..."嫦娥4号"任务将首次实现人类在月球背面软着陆。通过分析任务特点,以多类型有效载荷配置为背景,介绍了以科学目标和探测任务为核心的有效载荷系统设计思路和实现方法。同时针对首次在深空探测领域搭载国际合作有效载荷项目情况进行了说明。"嫦娥4号"任务最重要的科学目标是利用月球背面洁净的电磁环境进行天文低频射电观测,因此分别在着陆器和中继星上新增配置了国内新研制的低频射电频谱仪及荷兰研制的低频探测仪。科学探测的太阳爆发产生的低频电场信号极其微弱,如何消除着陆器和中继星上其他电子设备发射的近场噪声对远场探测信号的干扰就成了本次任务的最大难点。在相关研制单位的多方努力下,通过优化接收天线设计和地面数据处理算法等多种手段,实现了低频探测信号不低于30 d B的噪声抑制性能,具备了实现科学目标的能力。展开更多
To achieve the neutralization control requirements of the radio-frequency(RF)ion microthruster(μRIT)in the‘Taiji-1’satellite mission,we proposed an active neutralization control solution that is based on the carbon...To achieve the neutralization control requirements of the radio-frequency(RF)ion microthruster(μRIT)in the‘Taiji-1’satellite mission,we proposed an active neutralization control solution that is based on the carbon nanotube field emission technology.The carbon nanotube field emission neutralizer(CNTN)has the characteristics of light weight,small size,and propellantless,which is especially suitable for the neutralization control tasks of ion microthrusters.The Institute of Mechanics,Chinese Academy of Sciences,in collaboration with Tsinghua University,has successfully developed a CNTN to meet mission requirements.On the ground,the feasibility of cooperation working betweenμRIT and CNTN was fully verified,as well as the simulation and experimental study of neutralization control strategy,which finally passed the engineering assessment test.Since the launch of‘Taiji-1’satellite on 31 August,2019,the RF ion micropropulsion system has successfully completed nearly one hundred test missions in space.The test results indicate that CNTN does not have performance degradation,and the neutralization control strategy is effective.展开更多
文摘"嫦娥4号"任务将首次实现人类在月球背面软着陆。通过分析任务特点,以多类型有效载荷配置为背景,介绍了以科学目标和探测任务为核心的有效载荷系统设计思路和实现方法。同时针对首次在深空探测领域搭载国际合作有效载荷项目情况进行了说明。"嫦娥4号"任务最重要的科学目标是利用月球背面洁净的电磁环境进行天文低频射电观测,因此分别在着陆器和中继星上新增配置了国内新研制的低频射电频谱仪及荷兰研制的低频探测仪。科学探测的太阳爆发产生的低频电场信号极其微弱,如何消除着陆器和中继星上其他电子设备发射的近场噪声对远场探测信号的干扰就成了本次任务的最大难点。在相关研制单位的多方努力下,通过优化接收天线设计和地面数据处理算法等多种手段,实现了低频探测信号不低于30 d B的噪声抑制性能,具备了实现科学目标的能力。
基金supported by the Strategic Priority Research Program of the Chinese Academy of Sciences (Nos. XDB23030300, XDA1502070901, XDA1502070503)。
文摘To achieve the neutralization control requirements of the radio-frequency(RF)ion microthruster(μRIT)in the‘Taiji-1’satellite mission,we proposed an active neutralization control solution that is based on the carbon nanotube field emission technology.The carbon nanotube field emission neutralizer(CNTN)has the characteristics of light weight,small size,and propellantless,which is especially suitable for the neutralization control tasks of ion microthrusters.The Institute of Mechanics,Chinese Academy of Sciences,in collaboration with Tsinghua University,has successfully developed a CNTN to meet mission requirements.On the ground,the feasibility of cooperation working betweenμRIT and CNTN was fully verified,as well as the simulation and experimental study of neutralization control strategy,which finally passed the engineering assessment test.Since the launch of‘Taiji-1’satellite on 31 August,2019,the RF ion micropropulsion system has successfully completed nearly one hundred test missions in space.The test results indicate that CNTN does not have performance degradation,and the neutralization control strategy is effective.
