FIELD: military equipment, guided missiles. SUBSTANCE: air-dynamic unit of guided missile control actuator has actuation cylinder, distribution device and control electromagnet located in the body. Inclined fairings of exhaust ports changing into a cylindrical shoulder are made on the body. EFFECT: improved design. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1994 |
|
RU2066834C1 |
GUIDED MISSILE | 2005 |
|
RU2295698C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1997 |
|
RU2124697C1 |
GUIDED PROJECTILE | 1998 |
|
RU2150082C1 |
AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
CONTROL ACTIVATOR UNIT OF GUIDED MISSILE | 1998 |
|
RU2149345C1 |
GUIDED MISSILE CONTROL ACTUATOR | 1993 |
|
RU2072506C1 |
GUIDED MISSILE CONTROL ACTUATOR UNIT | 1995 |
|
RU2084810C1 |
ACTUATOR OF GUIDED PROJECTILE | 2004 |
|
RU2282134C2 |
Authors
Dates
1997-10-10—Published
1996-01-04—Filed