Show metadata Hide metadata

(19)

(11)

2 442 101

(13)

(51)

IPC

F42B12/44(2006-01-01)

F42B10/38(2006-01-01)

(21) (22)

Application

2010126812/11, 2010-06-30

(24)

Start date

2010-06-30

(22)

Actual filing date

2010-06-30

(45)

Published

2012-02-10

(72)

Inventor

Belobragin Boris AndreevichKaljuzhnyj Gennadij Vasil'EvichZakharov Oleg L'VovichKashirkin Aleksandr AleksandrovichZakharov Sergej OlegovichPetrov Valerij LeonidovichVan'Kov Viktor Timofeevich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Zavod Iskusstvennogo Volokna"

SUPERSONIC SPINNING MISSILE Russian patent published in 2012 - IPC F42B12/44 F42B10/38

Abstract RU 2442101 C1

FIELD: multiple rocket launcher ammunition.

SUBSTANCE: supersonic spinning missile comprises a warhead fitted with a container with fill liquid based on petroleum products and an air pocket, a jet motor and a stabiliser with sloping blades. The container with fill liquid and the air pocket has one or several tubular turbulators installed coaxially with the missile axis between the forward head and the aft head. The diameter of the turbulators is 0,05...0,15d, whereas the distance between the missile axis and the turbulator axis is 0,3...0,4d, where d is the inner diameter of the container.

EFFECT: mass-inertia misalignment caused by the motion of fill liquid and air pocket is eliminated, as both components mix into a homogeneous emulsion.

3 dwg

Similar patents RU2442101C1

Title	Year	Author	Number
HEAD PART OF VOLLEY FIRE ROCKET SYSTEM	2011	Belobragin Boris Andreevich Terekhov Bogdan Nikolaevich Zakharov Oleg L'Vovich Kashirkin Aleksandr Aleksandrovich Zakharov Sergej Olegovich Sporykhin Aleksandr Ivanovich Varenykh Nikolaj Mikhajlovich	RU2465542C1
SPIN-STABILIZED ROCKET	2000	Denezhkin G.A. Kadushkin A.I. Kaljuzhnyj G.V. Kuksenko A.F. Makarovets N.A. Minin V.A. Obozov L.I. Podchufarov V.I. Romanovtsev B.M. Semilet V.V. Uspenskij S.V.	RU2154799C1
SPIN-STABILIZED MISSILE	2001	Akel'Ev A.I. Belobragin B.A. Beznosov V.I. Denezhkin G.A. Dmitriev B.A. Makarovets N.A. Malakhov A.N. Obozov L.I. Romanovtsev B.M.	RU2195627C1
ROTATING MISSILE	2020	Alyazhedinov Vadim Rashitovich Belobragin Boris Andreevich Tregubov Viktor Ivanovich Bazarnyj Aleksej Nikolaevich Medvedev Vladimir Ivanovich Khlebnikov Igor Ivanovich Zakharov Oleg Lvovich Zakharov Sergej Olegovich Erokhin Vladimir Evgenevich Kuznetsov Vitalij Vasilevich Bykonya Igor Petrovich Mikhajlov Andrej Vladimirovich Khrykov Viktor Viktorovich Shatunova Natalya Nikolaevna	RU2732370C1
SPIN-STABILIZED ROCKET	2003	Makarovets N.A. Denezhkin G.A. Kaljuzhnyj G.V. Semilet V.V. Obozov L.I. Belobragin B.A. Shirokov V.V. Malakhov A.N. Beznosov V.I.	RU2248515C1
ROTATING ROCKET	2000	Belobragin B.A. Varenykh N.M. Denezhkin G.A. Kapchits A.A. Kuksenko A.F. Makarovets N.A. Obozov L.I. Romanovtsev B.M. Sporykhin A.I.	RU2174669C1
INCENDIARY NOSE CONE OF ROTATING ROCKET	2000	Belobragin B.A. Varenykh N.M. Denezhkin G.A. Dmitriev B.A. Kapchits A.A. Makarovets N.A. Obozov L.I. Romanovtsev B.M. Sporykhin A.I.	RU2174670C1
SPINNING MISSILE	2006	Makarovets Nikolaj Aleksandrovich Denezhkin Gennadij Alekseevich Semilet Viktor Vasil'Evich Kaljuzhnyj Gennadij Vasil'Evich Belobragin Boris Andreevich Shirokov Vladimir Vasil'Evich Terekhov Bogdan Nikolaevich Varenykh Nikolaj Mikhajlovich Sporykhin Aleksandr Ivanovich	RU2325612C1
NOZZLE UNIT OF SOLID-PROPELLANT ROCKER ENGINE WITH FITTED-ON STABILIZER UNIT	2001	Makarovets N.A. Denezhkin G.A. Semilet V.V. Kashirkin A.A. Peturkin D.M. Filatov V.G. Prolubnikov V.I. Bendrikovskij P.V.	RU2179651C1
TWO-STAGE ROLLING ROCKET	1996	Zhukov V.P. Kuznetsov V.M. Khripunov L.A.	RU2110755C1

RU 2 442 101 C1

Authors

Belobragin Boris Andreevich

Kaljuzhnyj Gennadij Vasil'Evich

Zakharov Oleg L'Vovich

Kashirkin Aleksandr Aleksandrovich

Zakharov Sergej Olegovich

Petrov Valerij Leonidovich

Van'Kov Viktor Timofeevich

Dates

2012-02-10—Published

2010-06-30—Filed