Cure shrink-resistant missile motor cases

Synthetic resins or natural rubbers -- part of the class 520 ser – Synthetic resins – Processes of preparing a desired or intentional composition...

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149 2, 523138, 523180, 523427, F42B 100, C09B 506, C06B 4510, C08K 515

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active

045159122

ABSTRACT:
Cure shrink-resistant missile motor cases are disclosed along with their method for construction. These cases comprise a matrix resin composition which includes a bisspiroortho carbonate as a fourth component, a curing agent of o-phenylenediamine boron trifluoride etherate as a third component, butanediol diglycidyl ether as a second component, and equal parts by weight of diglycidyl ether of bisphenol A and epoxidized dimer of oleic acid as a second component and additionally, they comprise, in combination therewith, a high strength fiber reinforcement material selected from the group consisting of fibers of glass, graphite, and poly-p-ethylene terephthalamide (Kevlar). The specific bisspiroortho carbonate which achieves an expansion of the matrix resin on polymerization or curing is 3,9-bis(5'-norbornene-2'-yl)-1,5,7,11-tetraoxaspiro [5.5]undecane. The expansion on curing prevents or decreases the inherent stress build-up in a fiber coated and filament wound composite motor case which is normally encountered when a standard matrix resin shrinks on polymerization or curing. A typical, standard resin includes the first two components and TONOX 60/40 which is a mixture comprised of 65% 4,4'-diaminodiphenylmethane, 10% triamines, and 25% polyamines.

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