RU93040952A - NON-ROTATING ARTILLERY SHELL - Google Patents

NON-ROTATING ARTILLERY SHELL

Info

Publication number
RU93040952A
RU93040952A RU93040952/23A RU93040952A RU93040952A RU 93040952 A RU93040952 A RU 93040952A RU 93040952/23 A RU93040952/23 A RU 93040952/23A RU 93040952 A RU93040952 A RU 93040952A RU 93040952 A RU93040952 A RU 93040952A
Authority
RU
Russia
Prior art keywords
projectile
rotating
artillery shell
battle
tail
Prior art date
Application number
RU93040952/23A
Other languages
Russian (ru)
Other versions
RU2046279C1 (en
Inventor
И.Ф. Горнев
В.П. Киреев
В.В. Михайлов
А.А. Хоничев
I.F. Gornev
V.P. Kireev
V.V. Mikhajlov
A.A. Khonichev
Original Assignee
Научно-исследовательский машиностроительный институт
Nauchno-Issledovatel'skij Mashinostroitel'nyj Institut
Filing date
Publication date
Application filed by Научно-исследовательский машиностроительный институт, Nauchno-Issledovatel'skij Mashinostroitel'nyj Institut filed Critical Научно-исследовательский машиностроительный институт
Priority to RU93040952A priority Critical patent/RU2046279C1/en
Priority claimed from RU93040952A external-priority patent/RU2046279C1/en
Application granted granted Critical
Publication of RU2046279C1 publication Critical patent/RU2046279C1/en
Publication of RU93040952A publication Critical patent/RU93040952A/en

Links

Claims (1)

Использование: в области артиллерийских снарядов, характеризующихся наличием кумулятивного или осколочно-фугасного заряда и оперения, раскрывающегося после выхода из ствола. Цель изобретения: создание конструкции снаряда с повышенной кучностью боя. Сущность изобретения: введение дополнительного стабилизирующего элемента, выполненного с кольцевой поверхностью, обращенной к нижней части снаряда, расположенной на сужающейся хвостовой части снаряда. Положительный эффект: кучность боя снаряда повышается на 20% - 30%.Usage: in the field of artillery shells, characterized by the presence of cumulative or high-explosive fragmentation charge and tail, drop-down after leaving the barrel. The purpose of the invention: the creation of the design of the projectile with increased accuracy of battle. The essence of the invention: the introduction of an additional stabilizing element, made with an annular surface facing the lower part of the projectile, located on the tapered tail of the projectile. Positive effect: the accuracy of the projectile battle increases by 20% - 30%.
RU93040952A 1993-08-12 1993-08-12 Non-rotating artillery shell RU2046279C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU93040952A RU2046279C1 (en) 1993-08-12 1993-08-12 Non-rotating artillery shell

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU93040952A RU2046279C1 (en) 1993-08-12 1993-08-12 Non-rotating artillery shell

Publications (2)

Publication Number Publication Date
RU2046279C1 RU2046279C1 (en) 1995-10-20
RU93040952A true RU93040952A (en) 1996-08-10

Family

ID=20146503

Family Applications (1)

Application Number Title Priority Date Filing Date
RU93040952A RU2046279C1 (en) 1993-08-12 1993-08-12 Non-rotating artillery shell

Country Status (1)

Country Link
RU (1) RU2046279C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU170322U1 (en) * 2016-04-21 2017-04-21 Акционерное общество "Новосибирский завод искусственного волокна" TWO MEDIUM Rocket Shell

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