Spacecraft orbiting artificial satellites and process for its de-orbiting artificial Earth satellite

摘要

1.the spacecraft u0434u043bu00a0 descent with the orbit of artificial earth satellite containing u0442u0435u043fu043bu043eu0438u0437u043eu043bu0438u0440u043eu0432u0430u043du043du044bu0435 corpus with u0437u0430u0442u0443u043fu043bu0435u043du043du043eu0439 nasal part, u0441u0442u0440u0435u043bu043eu0432u0438u0434u043du043eu0435 wing, ae u0440u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au0438u0435 and u0433u0430u0437u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au0438u0435 bodies stabilization and u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 space apparatus through pitch, hub and u0440u044bu0441u043au0430u043du044cu00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 in that it u0441u0442u0440u0435u043bu043e a prominent wing is established on the pattern of u0441u0440u0435u0434u043du0435u043fu043bu0430u043du0430,the surface of the shell and u043du0438u0436u043du00a0u00a0 spacecraft consists of a rear part and the front part of the specified length, u0441u043eu043fu0440u00a0u0436u0435u043du043du043eu0439 with u0437u0430u0442u0443u043fu043bu0435u043du043du043eu0439 nasal part and u0432u044bu043fu043eu043bu043du0435u043du043d oh such a form that u043fu0440u043eu0435u043au0446u0438u00a0 its vertical plane of symmetry of space apparatus forms a loop by decreasing towards the tail. u043du043au0446u0438u0435u0439,u043au0430u0441u0430u0442u0435u043bu044cu043du0430u00a0 which at its point u0441u043eu043fu0440u00a0u0436u0435u043du0438u00a0 with u0437u0430u0442u0443u043fu043bu0435u043du0438u0435u043c nasal part forms the angle to the front edge of the heating u0441u0442u0440u0435u043bu043eu0432u0438u0434u043du043eu0433u043e wing, u043fu0440u043eu0435u043au0446u0438u00a0 rear part on the same plane with a boundary line forms a circuit, u0441u043eu043fu0440u00a0u0436u0435u043du043du044bu0439 front, in u043fu043bu043eu0441u043au043eu0441u0442u00a0u0445, normal to the longitudinal axis of the space apparatus u043du0438u0436u043du00a0u00a0 surface has a profileat which point u0443u043fu043eu043cu00a0u043du0443u0442u043eu0433u043e contour in the plane of symmetry u0441u043eu043fu0440u00a0u0436u0435u043du044b with dots of the front edge of the wing and the points u0432u043eu0433u043du0443u0442u044bu043cu0438 u043bu0438u043du0438u00a0u043cu0438, monotonous in preset u0437u0440u0430u0441u0442u0430u044eu0449u0438u043cu0438 to front u043au0440u043eu043cu043au0430u043c wing u0444u0443u043du043au0446u0438u00a0u043cu0438.;2.method of launching spacecraft in orbit of artificial earth satellite containing u0442u0435u043fu043bu043eu0438u0437u043eu043bu0438u0440u043eu0432u0430u043du043du044bu0435 corpus with u0437u0430u0442u0443u043fu043bu0435u043du043du043eu0439 nasal part, u0441u0442u0440u0435u043bu043eu0432u0438u0434u043du043eu0435 cd u044bu043bu043e, aerodynamic bodies and u0433u0430u0437u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au0438u0435 stabilization and u0443u043fu0440u0430u0432u043bu0435u043du0438u00a0 space apparatus through pitch, hub and u0440u044bu0441u043au0430u043du044cu00a0 with stabilization and the office space by the through pitch.hub and u0440u044bu0441u043au0430u043du0438u00a0 on u0431u0430u043bu0430u043du0441u0438u0440u043eu0432u043eu0447u043du044bu0445 angles of attack under the influence of aerodynamic flow on the spacecraft, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 the u0433u0438u043fu0435u0440u0437u0432u0443u043au043eu0432u044bu0445 u0441u043au043eu0440u043eu0441u0442u00a0 x flight stabilization and office space by the pitch channel u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 on u0431u0430u043bu0430u043du0441u0438u0440u043eu0432u043eu0447u043du044bu0445 angles of attack for the u043eu0431u0442u0435u043au0430u043du0438u0435 wing u0430u044du0440u043eu0434u0438u043du0430 u043cu0438u0447u0435u0441u043au0438u043c education current flow lines with vectors of speedu0441u0442u0440u0435u043bu043eu0432u0438u0434u043du043eu0439 aimed primarily along the anterior edge of the wing.