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2 343 397

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(51)

IPC

F42B15/00(2006-01-01)

(21) (22)

Application

2006147023/02, 2006-12-27

(24)

Start date

2006-12-27

(22)

Actual filing date

2006-12-27

(45)

Published

2009-01-10

(72)

Inventor

Denezhkin Gennadij AlekseevichMakarovets Nikolaj AleksandrovichSemilet Viktor Vasil'EvichAljazhedinov Vadim RashitovichZakharov Oleg L'VovichVerbovenko Aleksandr AndreevichSavchenko Vladimir IvanovichBazarnyj Aleksej NikolaevichBatov Aleksandr Gennad'Evich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennoe Predprijatie

ROCKET MISSILE Russian patent published in 2009 - IPC F42B15/00

Abstract RU 2343397 C2

FIELD: weapons.

SUBSTANCE: invention concerns area of rocket technics, namely to rocket missiles of systems of a volley fire. In a rocket missile of an axis of blades are parallel to a longitudinal axis of a shell, and longitudinal axes snuffled are inclined to a longitudinal axis of a shell in a skew opposite direction forward edges of blades within the values defined under the formula: γ=(0.05...0.15) βd (H+d_st)/d_nb_o. Where - βa skew angle of edges of blades in a plane, perpendicular to edges, d - shell calibre, d_n - diameter of the circle which are passing through the centres of target sections of a jet engine nozzles, H - scope of blades of the stabiliser, d_st - diameter of the case of a shell in an installation site of blades of the stabiliser, b_o - an onboard chord of the blade.

EFFECT: increase of flying range, reliability of operation improvement of the characteristic of a compactness of a shell.

2 dwg

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RU 2 343 397 C2

Authors

Denezhkin Gennadij Alekseevich

Makarovets Nikolaj Aleksandrovich

Semilet Viktor Vasil'Evich

Aljazhedinov Vadim Rashitovich

Zakharov Oleg L'Vovich

Verbovenko Aleksandr Andreevich

Savchenko Vladimir Ivanovich

Bazarnyj Aleksej Nikolaevich

Batov Aleksandr Gennad'Evich

Dates

2009-01-10—Published

2006-12-27—Filed