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ExoMars2016火星探测计划进入、减速、着陆的验证任务分析

贾贺 荣伟

航天器工程2013,Vol.22Issue(4):109-115,7.
航天器工程2013,Vol.22Issue(4):109-115,7.DOI:10.3969/j.issn.1673-8748.2013.04.019

ExoMars2016火星探测计划进入、减速、着陆的验证任务分析

Review and Analysis of EDL Demonstrator Module of ExoMars 2016 Mission

贾贺 1荣伟1

作者信息

  • 1. 北京空间机电研究所,北京 100076
  • 折叠

摘要

Abstract

In this paper,we summarized the Entry,Decent,and Landing (EDL) technology of ESA's ExoMars 2016 Mission.The characteristics of EDL Demonstrator Module (EDM) are concluded in the paper.The key design points of the EDM are studied in detail,including mission structure,task object,mission planning,key technologies and so on.Combined with the current technology status of Mars exploration in China,a reasonable planing of the technologies for the Entry,Decent,Landing is need,and the relevant tests should be carried out timely.Firstly the development and validation of Entry,Decent,Landing platform for the entire Mars exploration shall be completed.Then an in-depth science mission to Mars shall be researched.The paper also can provide some references to making further study of the Mars exploration mission in the future.

关键词

ExoMars计划/火星探测/进入、减速、着陆/EDL验证器

Key words

ExoMars/Mars explore/Entry, Decent, and Landing (EDL)/EDL Demonstrator Module (EDM)

分类

航空航天

引用本文复制引用

贾贺,荣伟..ExoMars2016火星探测计划进入、减速、着陆的验证任务分析[J].航天器工程,2013,22(4):109-115,7.

基金项目

国家重大科技专项工程 ()

航天器工程

OACSTPCD

1673-8748

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