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航天器舱外载荷适配器技术综述

康永 周晖 马少君 高波 谭立

航天器工程2019,Vol.28Issue(2):104-111,8.
航天器工程2019,Vol.28Issue(2):104-111,8.DOI:10.3969/j.issn.1673G8748.2019.02.016

航天器舱外载荷适配器技术综述

Review of Spacecraft Exposed Payload Adapter Technology

康永 1周晖 1马少君 1高波 1谭立1

作者信息

  • 1. 兰州空间技术物理研究所,兰州 730000
  • 折叠

摘要

Abstract

The spacecraft exposed payload adapter is a small and light space docking mechanism. According to the mode of operation,the adapters are divided into passive and active types.The adapters of China and abroad,such as Japanese EEU (equipment exchange unit),American FRAM (flight releasable attachment mechanism)and so on,are introduced.Aiming at the probG lems of inaccurate positioning and insufficient driving force of manipulator operating and astronaut ergonomics,the key technologies and solutions of work mode,critical parts and ground experiment are analyzed.To meet the requirements of Chinese advanced payload tasks in the future,the active adapter with powerful functions and strong payloadGcarrying capacity should be studied.Aiming at the large high orbit spacecraft,the passive adapter technology should be studied.

关键词

轻小型空间对接机构/航天器舱外载荷适配器/引导定位/机械锁紧/人机工效学

Key words

light and small space docking mechanism/spacecraft exposed payload adapter/guiding and positioning/mechanical locking/astronaut ergonomics

分类

航空航天

引用本文复制引用

康永,周晖,马少君,高波,谭立..航天器舱外载荷适配器技术综述[J].航天器工程,2019,28(2):104-111,8.

航天器工程

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