SUPERSONIC MISSILE Russian patent published in 2023 - IPC F42B15/00 

Abstract RU 2799901 C1

FIELD: military equipment.

SUBSTANCE: invention relates to supersonic rockets and can be used to create multiple launch rocket systems. The supersonic rocket contains a pointed nose (1), a cylindrical body (2) and a tail block (3), including a nozzle block (4) and a bladed plumage (5). The leading edge of the bladed plumage (5) is displaced relative to the bevel (6) of the nozzle block (4) of the rocket in the direction of the pointed nose (1) by (0.6 to 0.9)(bo+d). The span of the bladed plumage (5) of the tail block (3) is (4.0 to 7.5)d2/a, where d is the calibre of the projectile; bo is the side chord bladed plumage; a is the length of the pointed nose.

EFFECT: stable flight along the entire trajectory with angles of attack not exceeding one degree, reducing the dispersion of projectiles and increasing the firing range due to the correct choice of the structural layout of the airframe.

1 cl, 1 dwg

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Authors

Vlasov Aleksej Vladimirovich

Zakharov Sergej Olegovich

Smirnov Aleksandr Vladimirovich

Borisov Oleg Grigorevich

Skorlupkin Dmitrij Borisovich

Evlanov Andrej Aleksandrovich

Khomyakov Evgenij Aleksandrovich

Dates

2023-07-13Published

2022-12-05Filed