ROCKET AERODYNAMIC RUDDER Russian patent published in 2014 - IPC F42B10/14 

Abstract RU 2520846 C1

FIELD: aircraft engineering.

SUBSTANCE: proposed rudder comprises airfoil arranged at rocket body to fold thereat and rudder control drive. Said rotary drive is arranged in rocket body wherein airfoil and interlock are fitted and locked. Said interlock comprises spring-loaded rocker in contact with said airfoil. Said airfoil represents a one-piece design. Tooth is made at one end of said rocker to contact with said airfoil. Control drive has arc-like groove to confine airfoil turn angles and cut-out to fit rocker opposite end in.

EFFECT: efficient control over rocket rudder.

6 dwg

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RU 2 520 846 C1

Authors

Shestakov Sergej Aleksandrovich

Zemskov Vjacheslav Aleksandrovich

Shapovalov Anatolij Ivanovich

Dates

2014-06-27Published

2013-03-29Filed