JPH0221100U - - Google Patents

Info

Publication number
JPH0221100U
JPH0221100U JP10013588U JP10013588U JPH0221100U JP H0221100 U JPH0221100 U JP H0221100U JP 10013588 U JP10013588 U JP 10013588U JP 10013588 U JP10013588 U JP 10013588U JP H0221100 U JPH0221100 U JP H0221100U
Authority
JP
Japan
Prior art keywords
spacecraft
docking
heat transfer
face
coupling
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP10013588U
Other languages
Japanese (ja)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP10013588U priority Critical patent/JPH0221100U/ja
Publication of JPH0221100U publication Critical patent/JPH0221100U/ja
Pending legal-status Critical Current

Links

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図はこの考案の1実施例を示す図、第2図
は従来の1実施例を示す図である。 図において、1は宇宙機aの端面、2は宇宙機
bの端面、3は結合装置a、4は結合装置b、5
はコネクタa、6はコネクタb、7は伝熱装置a
、8は伝熱装置bである。なお図中同一符号は同
一部分を示す。
FIG. 1 shows an embodiment of this invention, and FIG. 2 shows a conventional embodiment. In the figure, 1 is the end face of spacecraft a, 2 is the end face of spacecraft b, 3 is the coupling device a, 4 is the coupling device b, and 5
is connector a, 6 is connector b, 7 is heat transfer device a
, 8 is a heat transfer device b. Note that the same reference numerals in the figures indicate the same parts.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 第1の宇宙機と他の第2の宇宙機それぞれの端
面に取付けられ、両宇宙機を結合する結合装置と
、両宇宙機の信号や流体の出入をそれぞれ可能と
するためのコネクタ類とにより構成される1組の
ドツキング機構において、両宇宙機の結合動作中
に第1の宇宙機と第2の宇宙機の温度差を小さく
するための伝熱装置を具備したことを特徴とする
ドツキング機構。
A coupling device that is attached to the end face of the first spacecraft and the other second spacecraft and connects the two spacecraft, and connectors that enable signals and fluid to enter and exit the two spacecraft. A docking mechanism comprising a pair of docking mechanisms comprising a heat transfer device for reducing the temperature difference between a first spacecraft and a second spacecraft during a coupling operation of both spacecraft. .
JP10013588U 1988-07-28 1988-07-28 Pending JPH0221100U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10013588U JPH0221100U (en) 1988-07-28 1988-07-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10013588U JPH0221100U (en) 1988-07-28 1988-07-28

Publications (1)

Publication Number Publication Date
JPH0221100U true JPH0221100U (en) 1990-02-13

Family

ID=31327933

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10013588U Pending JPH0221100U (en) 1988-07-28 1988-07-28

Country Status (1)

Country Link
JP (1) JPH0221100U (en)

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