RU96118017A - MILITARY PART OF A HIGH-FIRE BREAKTHROUGH REACTIVE APPLIANCE - Google Patents

MILITARY PART OF A HIGH-FIRE BREAKTHROUGH REACTIVE APPLIANCE

Info

Publication number
RU96118017A
RU96118017A RU96118017/02A RU96118017A RU96118017A RU 96118017 A RU96118017 A RU 96118017A RU 96118017/02 A RU96118017/02 A RU 96118017/02A RU 96118017 A RU96118017 A RU 96118017A RU 96118017 A RU96118017 A RU 96118017A
Authority
RU
Russia
Prior art keywords
charge
appliance
reactive
shell
fragmentation
Prior art date
Application number
RU96118017/02A
Other languages
Russian (ru)
Other versions
RU2100764C1 (en
Inventor
М.И. Астахов
Г.А. Денежкин
В.Е. Ерохин
Г.В. Калюжный
Ю.А. Камчатников
Н.А. Макаровец
Г.И. Блинов
Б.М. Романовцев
В.В. Семилет
Original Assignee
Государственное научно-производственное предприятие "Сплав"
Filing date
Publication date
Application filed by Государственное научно-производственное предприятие "Сплав" filed Critical Государственное научно-производственное предприятие "Сплав"
Priority to RU96118017A priority Critical patent/RU2100764C1/en
Priority claimed from RU96118017A external-priority patent/RU2100764C1/en
Application granted granted Critical
Publication of RU2100764C1 publication Critical patent/RU2100764C1/en
Publication of RU96118017A publication Critical patent/RU96118017A/en

Links

Claims (1)

Боевая часть осколочно-фугасного действия реактивного снаряда, содержащая корпус, заряд взрывчатого вещества, расположенные между ними осколочные блоки и полость, примыкающую к торцевой части заряда, отличающаяся тем, что заряд снабжен оболочкой с возможностью ее вскрытия при давлении, не превышающем величину давления перехода горения заряда в детонацию, причем в полости, примыкающей к торцевой части заряда, а также между корпусом и участками оболочки заряда свободными от осколочных блоков, образованы разгрузочные камеры, которые соединены между собой газоводами и снабжены крышкой для сообщения с атмосферой, при этом часть разгрузочных камер выполнена в осколочных блоках.The warhead of a high-explosive fragmentation projectile containing a shell, explosive charge, fragmentation blocks located between them and a cavity adjacent to the end part of the charge, characterized in that the charge is provided with a shell with the possibility of opening it at a pressure not exceeding the combustion transition pressure the charge into detonation, and in the cavity adjacent to the end part of the charge, as well as between the body and the parts of the shell of the charge free from fragmentation blocks, unloading chambers are formed, which are connected Nena gazovodami interconnected and provided with a cover for communicating with the atmosphere, wherein a portion of the discharge chamber is formed in fission blocks.
RU96118017A 1996-09-16 1996-09-16 High-explosive fragmentation warhead of jet projectile RU2100764C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96118017A RU2100764C1 (en) 1996-09-16 1996-09-16 High-explosive fragmentation warhead of jet projectile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96118017A RU2100764C1 (en) 1996-09-16 1996-09-16 High-explosive fragmentation warhead of jet projectile

Publications (2)

Publication Number Publication Date
RU2100764C1 RU2100764C1 (en) 1997-12-27
RU96118017A true RU96118017A (en) 1998-03-10

Family

ID=20185287

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96118017A RU2100764C1 (en) 1996-09-16 1996-09-16 High-explosive fragmentation warhead of jet projectile

Country Status (1)

Country Link
RU (1) RU2100764C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2859899A (en) 1998-03-09 1999-09-27 Ildar Ibragimov Combustion chamber of the target active defeat device (variants)

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