MISSILE WITH AIR-JET ENGINE Russian patent published in 2016 - IPC F42B12/46 

Abstract RU 2585211 C1

FIELD: weapons and ammunition; rocketry.

SUBSTANCE: missile with air-jet engine comprises head air intake device which includes central body and shell, combustion chamber, gas generator, warhead, solid fuel starting engine and stabiliser with opening vanes. Shell is fixed on central body by means of longitudinal pylons, uniformly located in circumferential direction and installed at zero angle to longitudinal axis of rocket. Front edges of pylons are provided with symmetric tip with angle of 10°…30° and removed from air intake minimum passage flow section at distance of 0.5…3.0 of minimum clearance between shell and central body. Opening vanes are made arc-shaped, are directed by convex surfaces in direction of missile rotation.

EFFECT: increased missile range.

1 cl, 1 dwg

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RU 2 585 211 C1

Authors

Makarovets Nikolaj Aleksandrovich

Ivanov Igor Vladimirovich

Dolganov Mikhail Evgenevich

Smolyaga Vladimir Ivanovich

Stepanov Aleksej Vasilevich

Zakharov Sergej Olegovich

Bazarnyj Aleksej Nikolaevich

Maksimov Sergej Sergeevich

Ivankin Mikhail Anatolevich

Talyzin Vadim Alekseevich

Dates

2016-05-27Published

2015-05-13Filed