JPS4835601Y1 - - Google Patents

Info

Publication number
JPS4835601Y1
JPS4835601Y1 JP4396967U JP4396967U JPS4835601Y1 JP S4835601 Y1 JPS4835601 Y1 JP S4835601Y1 JP 4396967 U JP4396967 U JP 4396967U JP 4396967 U JP4396967 U JP 4396967U JP S4835601 Y1 JPS4835601 Y1 JP S4835601Y1
Authority
JP
Japan
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.)
Expired
Application number
JP4396967U
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 JP4396967U priority Critical patent/JPS4835601Y1/ja
Publication of JPS4835601Y1 publication Critical patent/JPS4835601Y1/ja
Expired legal-status Critical Current

Links

JP4396967U 1967-05-25 1967-05-25 Expired JPS4835601Y1 (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4396967U JPS4835601Y1 (ja) 1967-05-25 1967-05-25

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4396967U JPS4835601Y1 (ja) 1967-05-25 1967-05-25

Publications (1)

Publication Number Publication Date
JPS4835601Y1 true JPS4835601Y1 (ja) 1973-10-26

Family

ID=33217506

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4396967U Expired JPS4835601Y1 (ja) 1967-05-25 1967-05-25

Country Status (1)

Country Link
JP (1) JPS4835601Y1 (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016532809A (ja) * 2013-07-26 2016-10-20 エアバス ディフェンス アンド スペース エスアーエス ノズルの固定部および可動部間に密封装置を備えたロケットエンジン用燃焼ガス噴出ノズル

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016532809A (ja) * 2013-07-26 2016-10-20 エアバス ディフェンス アンド スペース エスアーエス ノズルの固定部および可動部間に密封装置を備えたロケットエンジン用燃焼ガス噴出ノズル

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