FIELD: rocket fuels.
SUBSTANCE: invention relates to rocket engineering and deals with epoxide molding composition for armoring channeled and channel-free inserted charges of mixed solid propellant with diameter 300-700 mm prepared by filling technique and operated within a large temperature range. Composition comprises 39-42% epoxide dian resin as modifier and plasticizer, 6.48-10.80% m-phenylenediamine as aromatic diamine, and 1.44-3.00% polyethylenepolyamine as aliphatic amine. Aromatic and aliphatic amines are taken at weight ratio 4.5:1.
EFFECT: improved technological, mechanical, and adhesion properties.
2 tbl, 7 ex
Title | Year | Author | Number |
---|---|---|---|
EPOXIDE MOULDING COMPOSITION FOR ARMORING OF INSERT CHARGE FROM MIX SOLID PROPELLANT | 2007 |
|
RU2377229C2 |
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|
RU2330832C1 |
EPOXIDE COMPOSITION | 2005 |
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RU2287003C1 |
METHOD OF MANUFACTURING REMOVABLE ARMORED SOLID MIXED PROPELLANT CHARGE | 2006 |
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RU2315741C1 |
METHOD OF PRODUCING AUXILIARY ARMORED CHARGE OF BALLISTIC ROCKET FUEL | 2007 |
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RU2345977C1 |
ADHESIVE COMPOSITION | 2015 |
|
RU2609479C1 |
REPAIR ADHESIVE COMPOSITION | 2009 |
|
RU2412973C1 |
COMPOUND | 2015 |
|
RU2613987C2 |
EPOXY COMPOSITION | 2003 |
|
RU2247133C2 |
POLYMER COMPOSITION FOR FILLING PIEZOCERAMIC TRANSMITTING-RECEIVING MODULES | 2013 |
|
RU2552740C2 |
Authors
Dates
2007-03-20—Published
2005-12-20—Filed