FIELD: polymer materials in rocket engineering.
SUBSTANCE: invention concerns process of producing heat-resistant epoxide compound for reinforced glass-fiber bodies used in fabrication of rigid armoring housings for removable charges of solid-fuel rocket engines. Compound is prepared by mixing 28-32% of epoxide dian resin having molecular mass 390-430, 28-32% of epoxide dian resin having molecular mass 480-540, and 14-18% of trimethylolpropane/epichlorohydrin condensation product, mixing being effected for 15-30 min at 80-100° C and stirrer rotation speed 125-158 rpm. When temperature drops to 60-80° C, mixture is supplemented by 24-27% of epoxycyanurate resin and stirred for further 15-30 min at stirrer rotation speed 125-158 rpm under residual pressure not higher than 20 mm Hg.
EFFECT: improved mechanical, adhesion, elastic, and working characteristics at higher vitrification temperature (135° C).
1 tbl, 6 ex
Title | Year | Author | Number |
---|---|---|---|
ARMOR COVER FOR INSERT CHARGE OF COMPOSITE SOLID PROPELLANT AND METHOD OF ITS MANUFACTURE | 2006 |
|
RU2336259C2 |
COLD-CURED EPOXY COMPOSITION | 2018 |
|
RU2749379C2 |
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|
RU2749380C2 |
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IMPREGNATING EPOXIDE BINDER FOR LOW-MODULE WINDING MATERIALS | 2005 |
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RU2287538C1 |
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RU2750222C2 |
BINDING COMPOSITION FOR IMPREGNATION OF REINFORCING MATERIAL AT ARMOURING OF SOLID PROPELLANT CHARGES BY WINDING METHOD | 2005 |
|
RU2310668C2 |
COMPOSITION FOR OBTAINING FOAM PLASTIC | 0 |
|
SU618384A1 |
POLYMER COMPOSITION | 2011 |
|
RU2528681C2 |
METHOD FOR PRODUCING HIGH-STRENGTH COMPOSITE REINFORCEMENT | 2022 |
|
RU2799001C1 |
Authors
Dates
2007-05-27—Published
2006-04-03—Filed