JPS4933839Y1 - - Google Patents

Info

Publication number
JPS4933839Y1
JPS4933839Y1 JP6736070U JP6736070U JPS4933839Y1 JP S4933839 Y1 JPS4933839 Y1 JP S4933839Y1 JP 6736070 U JP6736070 U JP 6736070U JP 6736070 U JP6736070 U JP 6736070U JP S4933839 Y1 JPS4933839 Y1 JP S4933839Y1
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
JP6736070U
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 JP6736070U priority Critical patent/JPS4933839Y1/ja
Publication of JPS4933839Y1 publication Critical patent/JPS4933839Y1/ja
Expired legal-status Critical Current

Links

JP6736070U 1970-07-07 1970-07-07 Expired JPS4933839Y1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6736070U JPS4933839Y1 (en) 1970-07-07 1970-07-07

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6736070U JPS4933839Y1 (en) 1970-07-07 1970-07-07

Publications (1)

Publication Number Publication Date
JPS4933839Y1 true JPS4933839Y1 (en) 1974-09-12

Family

ID=33235584

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6736070U Expired JPS4933839Y1 (en) 1970-07-07 1970-07-07

Country Status (1)

Country Link
JP (1) JPS4933839Y1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009504493A (en) * 2005-08-17 2009-02-05 エアバス・ドイチュラント・ゲーエムベーハー Attachment system and method for attaching the tail to the aircraft fuselage (continuous fuselage connection)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
USAF MODEL AIM-4D FALCON MISSILES=1970 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009504493A (en) * 2005-08-17 2009-02-05 エアバス・ドイチュラント・ゲーエムベーハー Attachment system and method for attaching the tail to the aircraft fuselage (continuous fuselage connection)

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