RU2005139877A - BINDING COMPOSITION FOR IMPREGNATING REINFORCING MATERIAL WHEN RESERVING CHARGES OF SOLID ROCKET FUEL BY WRAPPING METHOD - Google Patents

BINDING COMPOSITION FOR IMPREGNATING REINFORCING MATERIAL WHEN RESERVING CHARGES OF SOLID ROCKET FUEL BY WRAPPING METHOD Download PDF

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Publication number
RU2005139877A
RU2005139877A RU2005139877/02A RU2005139877A RU2005139877A RU 2005139877 A RU2005139877 A RU 2005139877A RU 2005139877/02 A RU2005139877/02 A RU 2005139877/02A RU 2005139877 A RU2005139877 A RU 2005139877A RU 2005139877 A RU2005139877 A RU 2005139877A
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RU
Russia
Prior art keywords
resin
reinforcing material
charges
solid rocket
reserving
Prior art date
Application number
RU2005139877/02A
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Russian (ru)
Other versions
RU2310668C2 (en
Inventor
Федор Сергеевич Красильников (RU)
Федор Сергеевич Красильников
Раиса Егоровна Албутова (RU)
Раиса Егоровна Албутова
Ольга Викторовна Артемова (RU)
Ольга Викторовна Артемова
Эдуард Федорович Охрименко (RU)
Эдуард Федорович Охрименко
Геннадий Васильевич Куценко (RU)
Геннадий Васильевич Куценко
Георгий Николаевич Амарантов (RU)
Георгий Николаевич Амарантов
Петр Кузьмич Колач (RU)
Петр Кузьмич Колач
Original Assignee
Федеральное государственное унитарное предпри тие"Научно-исследовательский институт полимерных материалов" (RU)
Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Application filed by Федеральное государственное унитарное предпри тие"Научно-исследовательский институт полимерных материалов" (RU), Федеральное государственное унитарное предприятие "Научно-исследовательский институт полимерных материалов" filed Critical Федеральное государственное унитарное предпри тие"Научно-исследовательский институт полимерных материалов" (RU)
Priority to RU2005139877/02A priority Critical patent/RU2310668C2/en
Publication of RU2005139877A publication Critical patent/RU2005139877A/en
Application granted granted Critical
Publication of RU2310668C2 publication Critical patent/RU2310668C2/en

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  • Epoxy Resins (AREA)
  • Reinforced Plastic Materials (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Claims (1)

Связующий состав для пропитки армирующего материала при бронировании зарядов твердого ракетного топлива методом обмотки, включающий эпоксидиановую смолу, изометилтетрагидрофталевый ангидрид, отличающийся тем, что он содержит сочетание эпоксидиановой смолы с молекулярной массой 390-430 с эпоксидиановой смолой с молекулярной массой 480-540, взятых в соотношении 1:1, и дополнительно содержит эпоксициануровую смолу, модифицированную продуктом конденсации триметилолпропана с эпихлоргидрином, при следующем соотношении компонентов, мас.%:A binder composition for impregnating a reinforcing material when booking solid rocket fuel charges by a winding method, including epoxy resin, isomethyl tetrahydrophthalic anhydride, characterized in that it contains a combination of epoxy resin with a molecular weight of 390-430 with an epoxy resin with a molecular weight of 480-540, taken in the ratio 1: 1, and additionally contains an epoxy cyanuric resin modified by the condensation product of trimethylolpropane with epichlorohydrin, in the following ratio, wt.%: эпоксидиановая смола с молекулярнойmolecular epoxidian resin   массой 390-430weighing 390-430 15,89-17,2915.89-17.29 эпоксидиановая смола с молекулярнойmolecular epoxidian resin   массой 480-540weighing 480-540 15,89-17,2915.89-17.29 эпоксициануровая смолаepoxy cyanide resin 13,62-14,8213.62-14.82 продукт конденсации триметилолпропанаtrimethylolpropane condensation product   с эпихлоргидриномwith epichlorohydrin 9,1-9,99.1-9.9 изометилтетрагидрофталевый ангидридisomethyl tetrahydrophthalic anhydride 40,7-45,540.7-45.5
RU2005139877/02A 2005-12-20 2005-12-20 Binding composition for impregnation of reinforcing material at armouring of solid propellant charges by winding method RU2310668C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005139877/02A RU2310668C2 (en) 2005-12-20 2005-12-20 Binding composition for impregnation of reinforcing material at armouring of solid propellant charges by winding method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005139877/02A RU2310668C2 (en) 2005-12-20 2005-12-20 Binding composition for impregnation of reinforcing material at armouring of solid propellant charges by winding method

Publications (2)

Publication Number Publication Date
RU2005139877A true RU2005139877A (en) 2007-06-27
RU2310668C2 RU2310668C2 (en) 2007-11-20

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RU2005139877/02A RU2310668C2 (en) 2005-12-20 2005-12-20 Binding composition for impregnation of reinforcing material at armouring of solid propellant charges by winding method

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Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2472826C1 (en) * 2011-06-27 2013-01-20 Открытое акционерное общество "Научно-исследовательский институт полимерных материалов" Thermoplastic armour composition for coating set-in charge of mixed slow-burning solid propellant
RU2540642C1 (en) * 2013-07-12 2015-02-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт химии и механики" (ФГУП "ЦНИИХМ") Method of obtaining organic thermally stable filling agent for thermo-erosion resistant armour jacket of mixed solid rocket propellant

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Publication number Publication date
RU2310668C2 (en) 2007-11-20

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Effective date: 20121221