Spacecraft and thermal resistance type end cap mounting structure thereof

The invention relates to a spacecraft and a thermal resistance type end cap mounting structure thereof. The structure comprises an end cap which is internally provided with a first thermal insulation piece, a rear cabin section, a second heat insulation piece which is arranged between the end cap an...

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Bibliographic Details
Main Authors LIU QING, XIAO RENQIN, HU SHANGANG, ZOU TIANPING, WANG QIAOYUN
Format Patent
LanguageChinese
English
Published 28.01.2022
Subjects
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