FIELD: weapon and ammunition.
SUBSTANCE: invention relates to missilery and applies to the production of the epoxide molding composition from the composite solid propellant by filling that is valid in a broad range of temperatures; the invention is aimed at armor planting of set-in grains, diameter of which varies from 300 to 700 mm. The composition includes the following proportion of the components, mass %: 27-36 of epoxy-diane resin ED-20, 3-5 of plasticiser-modifier of low-viscous epoxy diethyleneglycolic aliphatic resin DEG-1, 30-40 of amine hardening agent of low viscous polyamineimidozaline resin PO-300, 30-35 of alkylphenol interaction product gr. C9-C12 with chloromethyl oxirane.
EFFECT: increased of technical, elastic and mechanical properties of the composition.
2 tbl, 5 ex
| Title | Year | Author | Number |
|---|---|---|---|
| EPOXIDE MOULDING COMPOSITION FOR ARMORING OF INSERT CHARGE FROM MIX SOLID PROPELLANT | 2007 |
|
RU2377229C2 |
| EPOXIDE MOLDING COMPOSITION FOR ARMORING INSERTED CHARGES OF MIXED SOLID PROPELLANT | 2005 |
|
RU2295509C1 |
| EPOXIDE COMPOSITION | 2005 |
|
RU2287003C1 |
| PROCESS OF PRODUCTION OF HEAT-RESISTANT EPOXIDE COMPOUND FOR GLASS-FIBER MATERIALS | 2006 |
|
RU2299897C1 |
| ADHESIVE COMPOSITION | 2015 |
|
RU2609479C1 |
| METHOD OF PRODUCING AUXILIARY ARMORED CHARGE OF BALLISTIC ROCKET FUEL | 2007 |
|
RU2345977C1 |
| METHOD OF MANUFACTURING REMOVABLE ARMORED SOLID MIXED PROPELLANT CHARGE | 2006 |
|
RU2315741C1 |
| BINDING COMPOSITION FOR IMPREGNATION OF REINFORCING MATERIAL AT ARMOURING OF SOLID PROPELLANT CHARGES BY WINDING METHOD | 2005 |
|
RU2310668C2 |
| THERMOPLASTIC ARMOUR COMPOSITION FOR COATING SET-IN CHARGE OF MIXED SLOW-BURNING SOLID PROPELLANT | 2011 |
|
RU2472826C1 |
| POLYMER COMPOSITION | 2010 |
|
RU2458086C1 |
