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Information × Registration Number 0217U004288, 0115U000666 , R & D reports Title Implementation of a mathematical model of interaction between the mobile launcher with soil during the starting load popup.stage_title Head Kalashnikov Vyacheslav, Registration Date 30-01-2017 Organization Sumy State University popup.description2 The study subject – is an aircraft launching process on launch vehicles. The development object is a differential equation system of componental movement of launch vehicles and aircraft. The purpose of the work is a creating universal mathematical model for designating launch vehicles TBMS (TMS) and ground confunction characteristics during the short-term dynamic load. The research method – is classical methods of modern dynamics and methods of modelling. The results of existing structural scheme analysis of missile launch on launch vehicles are given. Analytic model of launch vehicles TBMS (TMS) and ground confunction during the short-term dynamic load are developed. Mathematical models of launch vehicles at mortar launch are created. The model of dynamic ground movement as elastic half-plane is developed. The movement of carrier-missile-container system during the mortar launch from transport and launch container together with consideration of container and ground dynamic confunction is analyzed. Forecasting assumption according to the study subject development – is a creating of information technology, as a set of design methods, construction activities and soft hardware, which are integrated for the purpose of obtaining, processing and using of information for technical and cost criteria of new equipment. Product Description popup.authors Авдєєва О.М. Васильєв А.В. Заскока А.М. Коплик І.В. Остапова О.П. Шийко О.М. popup.nrat_date 2020-04-02 Close