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- W1997272099 startingPage "1249" @default.
- W1997272099 abstract "The control of the burning rate is one of the important aspects in the extension of the capability of a solid propellant. The burning rate of a composite propellant was found to be increased remarkably by the proper impregnation of metallic foil, and upon the addition of a few percent of aluminum, silver and copper (in weight), the burning rate jumped up to several times that of the original one, providing there had been suitable processing. The impregnation of metallic foil was performed by mixing a predetermined amount of finely-cut strips of foil into propellant dough or by laminating the latter with foils. The propellant grain impregnated at random with strips of foil increased the burning rate considerably, but the one laminated with metallic foils which were oriented perpendicular to the burning surface showed the highest burning rate. The increment of the burning rate evidently depended upon the thickness of the foil used; the distance between adjacent foils for lamination showed no remarkable effe..." @default.
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- W1997272099 date "1967-05-01" @default.
- W1997272099 modified "2023-09-26" @default.
- W1997272099 title "On the Composite Solid Propellant Impregnated with Metallic Foil" @default.
- W1997272099 doi "https://doi.org/10.1246/bcsj.40.1249" @default.
- W1997272099 hasPublicationYear "1967" @default.
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