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Mechanical bond between a solid rocket propellant composition and a substrate and a method of effecting such a bond
Mechanical bond between a solid rocket propellant composition and a substrate and a method of effecting such a bond
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机译:固体火箭推进剂组合物与基材之间的机械结合以及实现这种结合的方法
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摘要
A mechanical bond between a solid rocket propellant composition and a substrate such as insulation material is provided by a quantity of molded member portions integral with the substrate and protruding from a substrate surface into the cured propellant composition whereby a linerless rocket motor may be provided. A method of effecting such a bond is also disclosed.
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