FIELD: aeronautical and mechanical engineering; manufacture of parts from structural materials, missile aerial fairings in particular.
SUBSTANCE: proposed material is used for manufacture of missile aerial fairings working at temperature of 900°C for a short period of time with no change in their radiotechnical characteristics. Proposed composite material on base of silicone dioxide contains sintered silicon dioxide, titanium silicone organic resin and modified epoxy resin whose molecule includes silicone and titanium atoms at the following ratio of components, mass-%: sintered silicone dioxide, 98.0-99.0 and silicone organic resin and modified epoxy resin at equal ratio, 1.0-2.0.
EFFECT: enhanced strength characteristics of material.
1 tbl, 3 ex
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR PRODUCTION OF COMPOSITE MATERIAL AND OBTAINED MATERIAL | 2004 |
|
RU2270180C2 |
| METHOD OF MAKING COMPOSITE MATERIAL BASED ON SINTERED SILICON DIOXIDE | 2007 |
|
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| METHOD OF PRODUCTION OF THE PROTECTIVE AND HARDENING LAYER IN THE SHELL OF THE ANTENNA BLISTER MADE OUT OF QUARTZ CERAMICS | 2004 |
|
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| METHOD OF MANUFACTURE OF ARTICLES FROM GLASS-REINFORCED PLASTICS | 2004 |
|
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| ELECTROCONDUCTIVE ADHESIVE | 2011 |
|
RU2466168C1 |
| METHOD OF PRODUCING COVER OF ANTENNA DOME OUT OF REACTION BONDED SILICON NITRIDE | 2010 |
|
RU2453520C1 |
| METHOD OF MAKING COVER OF ANTENNA CAP FROM QUARTZ CERAMIC | 2007 |
|
RU2345970C1 |
| METHOD OF PRODUCTION OF THE COMPOSITE HEAT-INSULATION MATERIAL AND THE MATERIAL MANUFACTURED BY THIS METHOD | 2005 |
|
RU2300509C2 |
| ROCKET NOSE ANTENNA CONE | 2002 |
|
RU2209494C1 |
| HEAT RESISTANT ADHESIVE COMPOSITION | 1992 |
|
RU2061727C1 |
