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GEP20063738B - Artillery Missile - Google Patents

Artillery Missile

Info

Publication number
GEP20063738B
GEP20063738B GEAP2002004804A GEP20063738B GE P20063738 B GEP20063738 B GE P20063738B GE AP2002004804 A GEAP2002004804 A GE AP2002004804A GE P20063738 B GEP20063738 B GE P20063738B
Authority
GE
Georgia
Prior art keywords
combustion chamber
parts
fuse
shell
missile
Prior art date
Application number
Inventor
Irodion Tabatadze
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 GEAP2002004804 priority Critical patent/GEP20063738B/en
Publication of GEP20063738B publication Critical patent/GEP20063738B/en

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Abstract

1. Technical Result Widening of functional capabilities. 2. Essence A missile comprises a hollow shell 1, which by the partition is divided into two parts, in one of the parts there is an opening 3 to place an explosive and a fuse 4 therein, and the second part has a form of a combustion chamber. The shell is tightly inserted into a case 12, a jet exit 9 of the combustion chamber is provided with a remote fuse 8 and a shield 10. 3. Field of Application Fighting equipment.
GEAP2002004804 2002-02-12 2002-02-12 Artillery Missile GEP20063738B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GEAP2002004804 GEP20063738B (en) 2002-02-12 2002-02-12 Artillery Missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GEAP2002004804 GEP20063738B (en) 2002-02-12 2002-02-12 Artillery Missile

Publications (1)

Publication Number Publication Date
GEP20063738B true GEP20063738B (en) 2006-01-25

Family

ID=45477773

Family Applications (1)

Application Number Title Priority Date Filing Date
GEAP2002004804 GEP20063738B (en) 2002-02-12 2002-02-12 Artillery Missile

Country Status (1)

Country Link
GE (1) GEP20063738B (en)

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