FIELD: engineering of devices for changing orientation of directional diagram of radiolocation station antenna, possible use in onboard target coordinators (homing heads) of controlled missiles.
SUBSTANCE: suspension support is utilized with roller bearing, size of which is increased up to size of antenna aperture, while only half of bearing is utilized, which is held directly to back side of antenna, in such a way, that rollers limit movement of internal casing of bearing in forward, backward and sideward directions.
EFFECT: increased area of support of bearings within limits up to dimensions of antenna aperture without decrease of aperture itself relatively to caliber of missile, thus making it possible to proportionally raise limit launching and radial overloads on missile, allowed for given construction of antenna support.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR CHANGING ORIENTATION OF DIRECTIONAL DIAGRAM | 2004 |
|
RU2282285C2 |
| DEVICE FOR CHANGING THE ORIENTATION OF THE FIELD OF VIEW OF A MISSILE HOMING HEAD | 2023 |
|
RU2810677C1 |
| OPTICAL-ELECTRONIC HOMING HEAD | 2024 |
|
RU2833954C1 |
| METHOD OF LONG-RANGE TARGET CAPTURE OF ZONE MISSILE HOMING HEAD AND LONG MISSILE GUIDANCE SYSTEM | 2015 |
|
RU2583347C1 |
| METHOD FOR EXPELLING MISSILE TO TRACK INITIATION AREA WITH TARGET SEEKING HEAD, AND SYSTEM FOR ITS IMPLEMENTATION (VERSIONS) | 2013 |
|
RU2542691C1 |
| METHOD FOR GENERATING INTERFERENCE OF THE “ANTIPODE” TYPE | 2021 |
|
RU2777922C1 |
| METHOD FOR DESTRUCTION OF MOVING TARGET BY GUIDED PROJECTILE WITH ACTIVE GUIDANCE SYSTEM AND PRE-ACCELERATION ENGINE | 1999 |
|
RU2151370C1 |
| GUIDED MISSILE | 1999 |
|
RU2164657C1 |
| PORTABLE SURFACE-TO-AIR MISSILE SYSTEM /VERSIONS/ | 2012 |
|
RU2514324C1 |
| AIRCRAFT LANDING SYSTEM | 1994 |
|
RU2086471C1 |
