GUIDED MISSILE Russian patent published in 2005 - IPC

Abstract RU 2248517 C2

FIELD: armament, in particular, rocketry.

SUBSTANCE: supporting bulges with grooves for outlet of the control surfaces are made on the frame of the guided missile in the area of arrangement of the control surfaces, a fairing is installed on their outer surface. The base with the components of the control actuator fastened on it is joined to the frame in the end face of the supporting bulges.

EFFECT: enhanced service reliability of the missile.

3 dwg

Similar patents RU2248517C2

Title	Year	Author	Number
CONTROL ACTUATOR UNIT OF GUIDED MISSILE	2005	Fimushkin Valerij Sergeevich Zybin Igor' Mikhajlovich Golovanov Nikolaj Sergeevich	RU2283470C1
GUIDED MISSILE	2005	Zybin Igor' Mikhajlovich Ovchelupov Nikolaj Vasil'Evich Fimushkin Valerij Sergeevich	RU2295698C1
GUIDED MISSILE ACTUATOR ASSEMBLY	1996	Babichev V.I. Zybin I.M. Fimushkin V.S.	RU2101666C1
GUIDED PROJECTILE STEERING DRIVE UNIT	2009	Stepanichev Igor' Veniaminovich Gusev Andrej Viktorovich Fimushkin Valerij Sergeevich Ovchelupov Nikolaj Vasil'Evich Alenichev Aleksandr Nikolaevich Kuznetsov Mikhail Jur'Evich	RU2399866C1
GUIDED MISSILE CONTROL ACTUATOR UNIT	1995	Zybin I.M. Fimushkin V.S. Kharitonov V.M.	RU2087841C1
METHOD OF OPENING CONTROL SURFACES OF GUIDED PROJECTILE ACTUATOR UNIT AND ACTUATOR UNIT FOR REALIZATION OF THIS METHOD	2002	Fimushkin V.S. Zybin I.M. Golovanov N.S. Nikanorov B.A.	RU2237598C2
GUIDED MISSILE NOSE CONE	1996	Zybin I.M. Fimushkin V.S.	RU2100767C1
CONTROL ACTUATOR UNIT OF GUIDED PROJECTILE	2004	Fimushkin Valerij Sergeevich Zybin Igor' Mikhajlovich Golovanov Nikolaj Sergeevich Ovchelupov Nikolaj Vasil'Evich	RU2280231C1
GUIDED MISSILE CONTROL ACTUATOR UNIT	1995	Babichev V.I. Zybin I.M. Fimushkin V.S. Kharitonov V.M.	RU2084810C1
GUIDED MISSILE	2004	Kuznetsov V.M. Zybin I.M. Fimushkin V.S.	RU2261414C1

RU 2 248 517 C2

Authors

Zybin I.M.

Fimushkin V.S.

Dates

2005-03-20—Published

2003-05-05—Filed