METHOD OF PRODUCING ROCKET BALLISTIC SOLID PROPELLANT CHARGE

摘要

FIELD: weapons. ^ SUBSTANCE: invention relates to rocket engineering. The proposed method comprises mixing propellant components up in a neutral medium, squeesing the propellant mass, rolling the said mass along with processing till molded mass, drying the latter and producing from it the charges using forming press. In mixing the aforesaid components in neutral medium, combustion inhibitor, i.e. gamma-polyoxymethylene with the mean grain size not exceeding 15.0 mu is added thereto. Note also that and nitrocelluloses is used with nitrogen content not exceeding 192.0 ml NO/g. ^ EFFECT: propellant combustion rate of 2,2 to 3,85 mm/s at Pk=40 kgf/cm2 and T=20°C. ^ 1 tbl