FIELD: weapons.
SUBSTANCE: transition device from missile nose cone ceramic jacket to missile case contains an adapter, connected to the jacket with an elastic compound, made from material, which is similar to the jacket material in linear expansion temperature coefficient in the given temperature range, annular fastening ledge. The device is additionally equipped with a course, made from viscoelastic material and located in the void, constituted by jacket surfaces, adjacent to the course, surface of adapter, support element and external delimiter of course movement. At that, support element and external delimiter of course movement are either made as a whole, or fixed to each other. Besides, they are a constituent part of adapter in the shape of ring with a bore in front butt end or in both butt ends. Supplementary course from viscoelastic material can be installed between rear butt end of the support element and the adapter.
EFFECT: increase of construction durability and manufacturability and decrease of weight.
2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
MISSILE NOSE CONE | 2007 |
|
RU2337437C1 |
COWL | 2018 |
|
RU2690051C1 |
ANTENNA FAIRING FOR HIGH-SPEED MISSILES | 2020 |
|
RU2733916C1 |
ANTENNA FAIRING | 2020 |
|
RU2735381C1 |
ANTENNA FAIRING | 2004 |
|
RU2277738C1 |
ANTENNA FAIRING | 2018 |
|
RU2690040C1 |
MISSILE NOSE FAIRING | 2010 |
|
RU2459325C1 |
FAIRING | 2017 |
|
RU2654953C1 |
DIRECTION-FINDING SYSTEM OF “ANTENNA-FAIRING” TYPE | 2020 |
|
RU2749384C1 |
CONE | 2002 |
|
RU2225664C2 |
Authors
Dates
2008-10-27—Published
2007-07-18—Filed