FIELD: guided missiles. SUBSTANCE: guided missile actuator assembly has control actuators with a distribution device and an air intake installed on the base. A manifold serving at the same time as a receiver is installed on the base between the leading shaped charge and the fairing. The air intakes are made rotary for outlet behind the fairing contours through the grooves for control surfaces and communicate with the manifold inlets through flexible tubes. A filter is installed inside the manifold, and the manifold outlet communicates with the inlet of the distribution device of the control actuators. EFFECT: improved design. 2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE | 2005 |
|
RU2295698C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2087841C1 |
GUIDED MISSILE NOSE CONE | 1996 |
|
RU2100767C1 |
GUIDED MISSILE NOSE CONE | 1995 |
|
RU2089834C1 |
CONTROL ACTUATOR UNIT OF GUIDED PROJECTILE | 2004 |
|
RU2280231C1 |
GUIDED MISSILE | 2003 |
|
RU2257533C1 |
GUIDED PROJECTILE | 1998 |
|
RU2150082C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2084810C1 |
GUIDED MISSILE | 1994 |
|
RU2084809C1 |
GUIDED MISSILE WARHEAD | 1994 |
|
RU2072504C1 |
Authors
Dates
1998-01-10—Published
1996-06-13—Filed