METHOD launching spacecraft into orbit artificial Earth satellite AND DEVICE FOR IMPLEMENTATION

摘要

1.way to the launch of a space u0430u0440u043fu0430u0440u0430u0442u0430 on orbit of artificial earth satellite, comprising a u0441u0435u0431u00a0 him the zero on the earth before the first space with the u043au043eu0440u043eu0441u0442u0438 carrier rocket, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 as the lead in two stages, the first stage uses the ground u043du0435u0440u0430u0437u0433u043eu043du00a0u0435u043cu044bu0439 together with u0437u0430u043fu0443u0441u043au0430u0435u043cu044bu043c u0430u043fu043fu0430u0440u0430u0442u043e m the source of energy for launching the device sufficient u043fu0440u043eu0442u00a0u0436u0435u043du043du043eu0441u0442u0438,to provide the apparatus with the permissible overloads to large speed and at a significant height above the surface of the earth, and in the second stage, u0440u0430u0437u0433u043eu043du00a0u044eu0442 apparatus to the required speed by a u043au043eu0442u043eu0440u0430u00a0 dispersed prior together with space machine at the first stage.;2. the device u0434u043bu00a0 pre disperse the spacecraft in the first stage, which u043du0430u043fu0440u0430u0432u043bu00a0u044eu0449u0438u0435 set at an angle to the horizon, u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 the fact that u043du0430u043fu0440u0430u0432u043bu00a0u044eu0449u0438u0435 implemented in the form of a linear u044du043bu0435u043au0442u0440u043eu0434u0432u0438u0433u0430u0442u0435u043bu00a0 and installed on the slope of mount elbrus in the direction of u0432u0440u0430u0449u0435u043du0438u00a0 land.