FIELD: rocketry; high-speed air-to-air missiles.
SUBSTANCE: novelty is that ceramic envelope made of void-free material that does not need moisture protection is joined with intermediate metal frame coordinated in temperature coefficient of linear expansion with envelope material by means of flexible heat-resistant adhesive applied to conical surfaces being joined. Intermediate frame is coaxially joined with attachment frame and its axial displacement is restricted on one end by means of two mating bosses provided on inner surface of attachment frame and on outer surface of intermediate frame and on other end, by pins press-fitted into attachment frame and installed in a spaced relation in blind holes of intermediate frame. Sealing ring is fitted in drilling at butt end of intermediate frame.
EFFECT: enhanced carrying capacity and reliability of antenna fairing.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HEAD ANTENNA DOME | 2016 |
|
RU2631917C1 |
| FAIRING | 2017 |
|
RU2654953C1 |
| ANTENNA FAIRING | 2022 |
|
RU2793304C1 |
| ANTENNA FAIRING | 2020 |
|
RU2735381C1 |
| ANTENNA FAIRING | 2001 |
|
RU2189673C1 |
| ANTENNA DOME | 2011 |
|
RU2464679C1 |
| FLYING-VEHICLE NOSE FAIRING | 2005 |
|
RU2280301C1 |
| CONE | 2002 |
|
RU2225664C2 |
| FAIRING | 2017 |
|
RU2650085C1 |
| MISSILE ANTENNA NOSE FAIRING | 2001 |
|
RU2189672C1 |
