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2 410 291

(13)

(51)

IPC

B64D27/02(2006-01-01)

F02K7/18(2006-01-01)

F42B15/00(2006-01-01)

(21) (22)

Application

2009141287/11, 2009-11-10

(24)

Start date

2009-11-10

(22)

Actual filing date

2009-11-10

(45)

Published

2011-01-27

(72)

Inventor

Malinin Vladimir Ignat'EvichVinogradov Sergej MikhajlovichIvanov Oleg MikhajlovichGureev Vladimir ValentinovichMarchenko Anatolij Iosifovich

(73)

Holder

Otkrytoe Aktsionernoe Obshchestvo Raketnoe Vooruzhenie"

SUPERSONIC MISSILE WITH POWDERED METALLIC FUEL ENGINE Russian patent published in 2011 - IPC B64D27/02 F02K7/18 F42B15/00

Abstract RU 2410291 C1

FIELD: engines and pumps.

SUBSTANCE: ultrasonic missile contains the body where there located is guidance system equipment, control system equipment, missile warhead, starting power plant and propulsion power plant. Air-intake devices and aerodynamic surfaces are located outside the body. Propulsion power plant is performed in a form of ramjet engine that consists of pre-combustion chamber and combustion chamber connected to air-intake devices and powdered metallic fuel supply system that uses a piston.

EFFECT: increase of flight range in larger flight altitude envelope.

2 cl, 1 dwg

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RU 2 410 291 C1

Authors

Malinin Vladimir Ignat'Evich

Vinogradov Sergej Mikhajlovich

Ivanov Oleg Mikhajlovich

Gureev Vladimir Valentinovich

Marchenko Anatolij Iosifovich

Dates

2011-01-27—Published

2009-11-10—Filed