ROCKET Russian patent published in 2007 - IPC F42B15/00 

Abstract RU 2295697 C1

FIELD: armament.

SUBSTANCE: the rocket has a subcaliber sustainer stage with fairing blades fastened on its body, and a separable engine telescope joined to the aft of the sustainer stage body. Flaps made with longitudinal grooves enveloping the trailing edges of the fairing blades are hinge-joined on the trailing edges of the fairing blades near the board chord. The engine front section is provided with bearing surfaces for engagement with the bearing surfaces of the flaps, they are made for engagement with the bearing surfaces of the flaps positioned in parallel with the trailing edges of the fairing blades.

EFFECT: enhanced operating characteristics of the rocket.

5 dwg

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RU 2 295 697 C1

Authors

Kuznetsov Vladimir Markovich

Zhukov Vladimir Petrovich

Alekseev Aleksandr Nikolaevich

Korneichev Aleksandr Vjacheslavovich

Dates

2007-03-20Published

2005-09-05Filed