FIELD: weapons.
SUBSTANCE: group of inventions is related to rocket engineering and may be used in guided missiles and projectiles of precision weapons complexes. Missile contains air vanes that open through longitudinal slots of casing, electromagnet shield. Shield is made in form of aluminium foil segments, which are located on external surface of casing above slots and fixed to sealing cover sheets and to casing along perimeter of slots with dielectric glue composition. Method includes installation of sealing cover sheets into slots and casing painting. Prior to painting slots are insulated with segments of aluminium foil, by their fixation to external surfaces of cover sheets and casing with dielectric glue composition.
EFFECT: provision of protection of missile control system electric circuits against external electromagnet fields.
2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED ARTILLERY PROJECTILE | 2004 |
|
RU2258897C1 |
| GUIDED PROJECTILE STEERING DRIVE UNIT | 2009 |
|
RU2399866C1 |
| METHOD FOR CONTROL OF SPIN-STABILIZED MISSILE AND GUIDED MISSILE | 2004 |
|
RU2275584C2 |
| CONTROL ACTUATOR UNIT OF GUIDED MISSILE | 2005 |
|
RU2283470C1 |
| CONTROLLED PROJECTILE, STEERING DRIVE GROUP OF CONTROLLED PROJECTILE, PNEUMATIC DISTRIBUTION DEVICE OF STEERING DRIVE OF CONTROLLED PROJECTILE, MECHANISM OF INITIATION OF STEERING DRIVE OF CONTROLLED PROJECTILE | 2017 |
|
RU2669979C1 |
| METHOD OF OPENING CONTROL SURFACES OF GUIDED PROJECTILE ACTUATOR UNIT AND ACTUATOR UNIT FOR REALIZATION OF THIS METHOD | 2002 |
|
RU2237598C2 |
| ARTILLERY SHELL STEERING DRIVE UNIT | 2023 |
|
RU2825788C1 |
| GUIDED MISSILE ACTUATOR ASSEMBLY | 1996 |
|
RU2101666C1 |
| AIR-DYNAMIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 1996 |
|
RU2092782C1 |
| UNIT OF STEERING DRIVE OF ARTILLERY SHELL | 2000 |
|
RU2175431C1 |
