航天器工程2019，Vol.28Issue(1)：84-89,6.DOI:10.3969/j.issn.1673-8748.2019.01.012
上面级直接入轨卫星星箭供电接口设计与验证
Design and Validation of Power Interface Between Direct Inj ection Satellites and Upper Stages
摘要
Abstract
In order to meet the demand of the energy consumption of direct inj ection satellites on the upper stages,this paper presents the restraint of the common design of power interface.The design of the power interface between two satellites and the upper stage has been presented ac-cording to power topological structure,batteries and the safety of power supply,then the conclu-sion of the practical appearance has been made.The design meets the energy demand of the satel-lite which is more than 5 hours before separation between satellites and upper stage.The conclu-sion provide the reference to all kinds of power interfaces between direct inj ection satellites and upper stages,solving the problem of power using on the transfer orbit and also improving effi-ciency and reliability.关键词
上面级/直接入轨卫星/星箭供电接口/转移轨道Key words
upper stage/direct inj ection satellite/satellite-rocket power interface/transfer orbit分类
航空航天引用本文复制引用
陈世杰,孙世卓,付大伟,曾毅..上面级直接入轨卫星星箭供电接口设计与验证[J].航天器工程,2019,28(1):84-89,6.基金项目
国家重大航天工程 （）
