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2 299 397

(13)

(51)

IPC

F42B15/00(2006-01-01)

(21) (22)

Application

2006117432/02, 2006-05-23

(24)

Start date

2006-05-23

(22)

Actual filing date

2006-05-23

(45)

Published

2007-05-20

(72)

Inventor

Makarovets Nikolaj AleksandrovichDenezhkin Gennadij AlekseevichSemilet Viktor Vasil'EvichTregubov Viktor IvanovichKoroleva Natal'Ja BorisovnaPeturkin Dmitrij MikhajlovichKashirkin Aleksandr AleksandrovichPetrov Valerij LeonidovichVan'Kov Viktor Timofeevich

(73)

Holder

Federal'Noe Gosudarstvennoe Unitarnoe Predprijatie Zavod Iskusstvennogo Volokna"

ROCKET Russian patent published in 2007 - IPC F42B15/00

Abstract RU 2299397 C1

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

SUBSTANCE: the rocket has a nose cone, solid-propellant rocket engine, stabilizer unit. The rear edges of the stabilizers in the area of the root chord are positioned at a distance of 0.5 to 0.7 of the diameter of the nozzle exit section. The nozzle subsonic section is made with an angle of 15 to 25 deg. The thickness of the nozzle subsonic section heat-resisting coating makes up 1.2 to 4 of the nozzle supersonic section heat-resisting coating.

EFFECT: makes it possible to produce a rocket with an improved accuracy and closely grouped fire.

2 dwg

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RU 2 299 397 C1

Authors

Makarovets Nikolaj Aleksandrovich

Denezhkin Gennadij Alekseevich

Semilet Viktor Vasil'Evich

Tregubov Viktor Ivanovich

Koroleva Natal'Ja Borisovna

Peturkin Dmitrij Mikhajlovich

Kashirkin Aleksandr Aleksandrovich

Petrov Valerij Leonidovich

Van'Kov Viktor Timofeevich

Dates

2007-05-20—Published

2006-05-23—Filed