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2 319 106

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(51)

IPC

F42B15/00(2006-01-01)

(21) (22)

Application

2006121118/02, 2006-06-13

(24)

Start date

2006-06-13

(22)

Actual filing date

2006-06-13

(45)

Published

2008-03-10

(72)

Inventor

Makarovets Nikolaj AleksandrovichDenezhkin Gennadij AlekseevichSemilet Viktor Vasil'EvichKashirkin Aleksandr AleksandrovichKaljuzhnyj Gennadij Vasil'EvichVan'Kov Viktor TimofeevichPetrov Valerij LeonidovichAljazhedinov Vadim RashitovichKoroleva Natal'Ja BorisovnaTregubov Viktor Ivanovich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Nauchno-Proizvodstvennoe Predprijatie

MISSILE Russian patent published in 2008 - IPC F42B15/00

Abstract RU 2319106 C1

FIELD: rocketry, in particular, missiles of salvo-fire jet systems.

SUBSTANCE: the missile has a nose cone, section of attitude stabilization gaseous jet system with nozzles in the area of the cylindrical section and with a cylindrical insert charge, the axes of the nozzles are located in the missile cross-section being apart from the joint with the tapered or ogival section at distance (6-7)d, and from the conjugate point with the adjacent cylindrical section at distance (2-3)d, where d-the diameter of the nozzle outlet section.

EFFECT: improved closely-ground fire due to reduction of the spread of the control forces of the attitude stabilization gaseous jet system.

1 dwg

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RU 2 319 106 C1

Authors

Makarovets Nikolaj Aleksandrovich

Denezhkin Gennadij Alekseevich

Semilet Viktor Vasil'Evich

Kashirkin Aleksandr Aleksandrovich

Kaljuzhnyj Gennadij Vasil'Evich

Van'Kov Viktor Timofeevich

Petrov Valerij Leonidovich

Aljazhedinov Vadim Rashitovich

Koroleva Natal'Ja Borisovna

Tregubov Viktor Ivanovich

Dates

2008-03-10—Published

2006-06-13—Filed