FIELD: aircraft industry; superhigh-speed flying vehicles. SUBSTANCE: proposed antenna fairing for air-to-surface missile has ceramic envelope joined to metal frame by means of elastic adhesive through additional intermediate envelope mounted inside fairing in a spaced relation and made of composite material consistent in ТКЛР with ceramic envelope material. Nose part of additional envelope is bonded by means of elastic adhesive to ceramic envelope through flexible cowling and to metal supporting ring installed on its inner surface. Flexible gasket is fitted between butt-joining flange of frame and end of ceramic envelope; additional flexible cowling is placed in annular drilling of frame at butt-joining flange to join ceramic envelope with frame by means of adhesive. EFFECT: improved performance characteristics meeting advanced specifications. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ANTENNA NOSE FAIRING | 2004 |
|
RU2273077C1 |
ROCKET NOSE CONE | 2000 |
|
RU2168815C1 |
ANTENNA FAIRING | 2001 |
|
RU2189674C1 |
ANTENNA FAIRING | 2001 |
|
RU2189673C1 |
CONE | 2002 |
|
RU2225664C2 |
ROCKET NOSE CONE | 2004 |
|
RU2269845C1 |
ANTENNA FAIRING | 2004 |
|
RU2277738C1 |
MISSILE NOSE FAIRING | 2010 |
|
RU2459325C1 |
ANTENNA FAIRING FOR HIGH-SPEED MISSILES | 2020 |
|
RU2733916C1 |
HEAD ANTENNA DOME | 2016 |
|
RU2631917C1 |
Authors
Dates
2002-09-20—Published
2001-06-15—Filed