Method of transportation into space and return trip OBJECTS complex configuration hypersonic RAKETOSTAT FOR IMPLEMENTATION

摘要

1.way of transportation in space and u0432u043eu0437u0432u0440u0430u0449u0435u043du0438u00a0 back of complex configuration, in which a carrier in the form of a thin u0432u044bu043fu043eu043bu043du00a0u044eu0442 u043eu0431u043eu043bu043eu0447u0435u0447u043du043eu0439 constructions, for instance r in the form of u0434u0438u0440u0438u0436u0430u0431u043bu00a0 or upwards, u0437u0430u043fu043eu043bu043du00a0u0435u043cu043eu0439 gaseous hydrogen producing static producing, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, after u0434u043eu0441u0442u0438u0436u0435u043du0438u00a0 u0430u044du0440u043eu0441u0442u0430u0442u043eu043c or with its load of setting of the maximum height of liftwhere u043eu0431u0435u0441u043fu0435u0447u0438u0432u0430u0435u0442u0441u00a0 minimum aerodynamic resistance through the center, gaseous hydrogen are heated, for example, by u044du043bu0435u043au0442u0440u0438u0447u0435u0441u043a oh, dougie, u00a0u0434u0435u0440u043du043eu0439 power installation or u0441u0436u0438u0433u0430u00a0, combining it with gaseous oxygen, and project through the nozzle in the direction opposite vector sc u043eu0440u043eu0441u0442u0438 disperse, the necessary u0434u043bu00a0 withdrawal object in spacethe received response u0442u00a0u0433u0443 is used as a main or auxiliary u0434u043bu00a0 withdrawal of objects in space, such as the earth's orbit, while diri u0436u0430u0431u043bu044e or u0430u044du0440u043eu0441u0442u0430u0442u0443 attached to the aerodynamic u043eu0431u0442u0435u043au0430u0435u043cu0443u044e form, and the thermal stress caused by the u043eu0431u0442u0435u043au0430u043du0438u0435u043c u043du0430u0431u0435u0433u0430u044eu0449u0435u0433u043e air flow to disperse in the atmosphere at finding an object in spaceand in u0432u0440u0435u043cu00a0 his u0442u043eu0440u043cu043eu0436u0435u043du0438u00a0 in dense u0441u043bu043eu00a0u0445 atmosphere re-entry, filming, u043eu0431u0435u0441u043fu0435u0447u0438u0432u0430u00a0 continuous u0446u0438u0440u043au0443u043bu00a0u0446u0438u044e the gas inside the shell u0434u0438u0440u0438u0436u0430u0431u043bu00a0 il and upwards, with u0434u043bu00a0 u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 more effective active u0442u0435u043fu043bu043eu0437u0430u0449u0438u0442u044b and u0443u043cu0435u043du044cu0448u0435u043du0438u00a0 quantity of gas necessary u0434u043bu00a0 u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 u0446u0438u0440u043au0443u043bu00a0u0446u0438u0438 inside u043eu0431u043eu043bu043eu0447u043a and, theit u0432u044bu043fu043eu043bu043du00a0u044eu0442 multilayer (double) with u043cu0435u0436u043eu0431u043eu043bu043eu0447u0435u0447u043du044bu043c space and serve the circulating gas, for example, the compressor in the u043cu0435u0436u043eu0431u043eu043bu043eu0447u0435u0447u043du043eu0435 space and beneath u0433u0440u0435u0442u044bu0439 gas due to u0432u0437u0430u0438u043cu043eu0434u0435u0439u0441u0442u0432u0438u00a0 with hot shell, u0440u0430u0441u0448u0438u0440u00a0u00a0u0441u044c and u043du0430u0433u0440u0435u0432u0430u00a0u0441u044c partly compensates the loss of u0434u0430u0432u043bu0435u043du0438u00a0 and reducing static lifting force in his u0440u0430u0441u0445u043eu0434u0435 to create reactive u0442u00a0u0433u0438,the braking when entering the atmosphere of planets u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 u0440u0430u0441u043fu0440u0430u0432u043bu0435u043du043du043eu0439 through internal u0434u0430u0432u043bu0435u043du0438u00a0 or shell, shell made of refractory materials sr, for example of a titanium foil, steel or u043fu043eu043bu0438u0438u043cu0438u0434u043du043eu0439 films (u043au0430u043fu0442u043eu043du0430), in u0446u0435u043bu00a0u0445 u0443u043cu0435u043du044cu0448u0435u043du0438u00a0 unit load at the maximum of its use square and the lift to drag ratio.u0434u043bu00a0 u0442u043eu0440u043cu043eu0436u0435u043du0438u00a0 which u0441u043eu0431u043bu044eu0434u0430u0435u0442u0441u00a0 attitude of return from space object to the bearing shell in the range in which the temperature u043du0430u0433u0440u0435 wa material shell does not exceed the temperature of its u0440u0430u0437u0440u0443u0448u0435u043du0438u00a0). 350 - 1000u0441).when the unit load is within 0.1 - 10 kg / m2, in addition large objects of complex shape, such as solar power plants, space mirrors or orbital station, u0432u044bu0432u043eu0434u00a0u0442 from the planet's surface without the process of (u0441u043au043bu0430u0434u044bu0432u0430u043du0438u00a0) in assembled form.u0434u043bu00a0 which create large sealed internal cavity of their design and the space u0437u0430u043fu043eu043bu043du00a0u044eu0442 gaseous hydrogen or provided with u043du0435u043eu0431u0445u043eu0434u0438u043cu043eu0441 t additional hermetic shell, which u0437u0430u043fu043eu043bu043du00a0u044eu0442 hydrogen and use static force u0434u043bu00a0 recovery in the upper atmosphere, where its resistance to mi u043du0438u043cu0430u043bu044cu043du043e,with the u043eu0441u0443u0449u0435u0441u0442u0432u043bu00a0u044eu0442 through jet streams punk hydrogen gas from domestic empty spaces u0432u044bu0432u043eu0434u0438u043cu043eu0439 structure and liquid u0440u0430u043au0435u0442u043d s engines with additional supplies of liquid propellant.;2. method for p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, however, that large flat surface space reflectors and photovoltaic power plants collect space on the planet's surface in the e situation and use them as part of a hermetic shell, with the shell of data objects u043du0430u0445u043eu0434u0438u0442u0441u00a0 inside the hermetic space filled with gaseous hydrogen.the working plane is formed between u0440u0435u0444u043bu0435u043au0442u043eu0440u0430 and further a hermetic shell, and the large area after u0441u0442u0430u0442u0438u0447u0435u0441 flat structures who up to the start u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 height in a direction parallel to their planes (rib to flow).;3. method for p.2, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, parabolic u0440u0435u0444u043bu0435u043au0442u043eu0440u044b u0432u044bu0432u043eu0434u00a0u0442 into space in the form of u0434u043bu00a0 parchment, which supply the casings membrane, the space between the kotor a u0437u0430u043fu043eu043bu043du00a0u044eu0442 gaseous hydrogen, with a circumference of the ring forms the power rim frame, to which u043au0440u0435u043fu00a0u0442 from two sides of membrane in the form of certain and the metal foil or u0442u043eu043du043au043eu043fu043bu0435u043du043eu0447u043du043eu0433u043e materialthe space between the u0437u0430u043fu043eu043bu043du00a0u044eu0442 hydrogen and the reactive u0442u00a0u0433u0443 u0441u0438u043bu043eu0432u043eu043cu0443 make to ring, the main rocket u0434u0432u0438u0433u0430u0442u0435u043bu00a0 and propellant u0434u043bu00a0 them, r u0430u0437u043cu0435u0449u0430u044eu0442 on the power ring.;4. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 2, so that the ring u043eu0431u0438u0442u0430u0435u043cu0443u044e space station with artificial gravity, such as the space station or interplanetary u043fu0438u043bu043eu0442u0438u0440u0443u0435 organization system, constructed in the shape of u0442u043eu0440u043eu0438u0434u0430, u0432u044bu0432u043eu0434u00a0u0442 into space in the same way as parabolic u0440u0435u0444u043bu0435u043au0442u043eu0440u044b and u043eu0431u0438u0442u0430u0435u043cu0443u044e station is used as a power u043au043eu043bu044cu0446 eva shell.;5. method for p.3, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u043eu0431u0438u0442u0430u0435u043cu0443u044e space station u0432u044bu043fu043eu043bu043du00a0u044eu0442 reflectors in the form of radio, with one of the two membranes u0432u044bu043fu043eu043bu043du00a0u044eu0442 from material u0438u043cu0435u044eu0449u0435u0433 on the u043eu0442u0440u0430u0436u0430u0442u0435u043bu044cu043du044bu0435 properties in a radio or optical range, and the other of the transparent data ranges of material, and after the u0437u0430u043fu043eu043bu043du0435u043du0438u00a0 hydrogen spaces and u043eu0431u0440u0430u0437u0443u0435u0442u0441u00a0 u0434u0432u043eu00a0u043au043eu0432u044bu043fu0443u043au043bu044bu0439 paraboloid u0432u0440u0430u0449u0435u043du0438u00a0,with a focus on the side of the transparent part of the shell, and u0434u043bu00a0 u0441u043eu0445u0440u0430u043du0435u043du0438u00a0 radio forms after u043fu0440u043eu0431u043eu00a0 meteor transparent and u0440u0435u0444u043bu0435u043au0442u043eu0440u043du0443u044e shell u0437u0430u0440u00a0u0436 u0430u044eu0442 identical electric or electrostatic u0437u0430u0440u00a0u0434u0430u043cu0438, if the height of u043du0435u0431u043eu043bu044cu0448u0430u00a0 hoops, or different u0437u0430u0440u00a0u0434u0430u043cu0438, if the height of u0431u043eu043bu044cu0448u0430u00a0 hoops, with u043fu0430u0440u0430u0431u043eu043b u043eu0438u0434 of two membranes takes u0434u0432u043eu00a0u043au043eu0432u043eu0433u043du0443u0442u0443u044e form.;6. method for p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that, with a view to u043fu0440u0438u0434u0430u043du0438u00a0 additional growth speed in an arbitrary slope, flat design in terms of form, for example, plo the partnership u0440u0435u0444u043bu0435u043au0442u043eu0440u044b or space stations, as well as u0434u0432u043eu00a0u043au043eu0432u044bu043fu0443u043au043bu044bu0435 or u0432u044bu043fu0443u043au043bu043eu0432u043eu0433u043du0443u0442u044bu0435 design with power rim in the form of a ring and the two membranes.point angle to vertical flow in the vertical gradient of the design, with an aerodynamic lifting force vector has a gore u0438u0437u043eu043du0442u0430u043bu044cu043du043eu0435 direction aimed in the direction of flight.;7. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that large orbital and interplanetary station manned spacecraft are collected in a single complex on earth (planet) and u0437u0430u043fu043eu043bu043du00a0u044eu0442 herm u0435u0442u0438u0447u043du044bu0435 internal cavity u043fu043eu043cu0435u0449u0435u043du0438u00a0 and gaseous hydrogen, helium or air u0433u043eu0440u00a0u0447u0438u043c create static producing.;8. method for p.4, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that, with a view to u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 heavy missile launchers by u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 their size, as well as u0434u043bu00a0 u0443u043cu0435u043du044cu0448u0435u043du0438u00a0 loads from large masses of warm wa at the bottom of missiles and rocket engines to high u0440u0430u0441u0441u0442u043eu00a0u043du0438u00a0 from each other, u0434u043bu00a0 u0443u043cu0435u043du044cu0448u0435u043du0438u00a0 their mutual u0432u043bu0438u00a0u043du0438u00a0 in u0430u043au0443u0441u0442u0438u0447u0435u0441u043au043eu043c and u0432u0438u0431u0440u043eu0434u0438u0430u043fu043eu0437u043eu043du0430u0445, rocket launcher u0432u044bu043fu043eu043bu043du00a0u044eu0442 u0442u043eu0440u043eu0438u0434u0430u043bu044cu043du043eu0439 formand u0434u043bu00a0 u0443u043cu0435u043du044cu0448u0435u043du0438u00a0 frontal u0441u043eu043fu0440u043eu0442u0438u0432u043bu0435u043du0438u00a0 on the flight with the u0430u044du0440u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au0438u043cu0438 loads u0442u043eu0440u043eu0438u0434u0443 attached u0432u044bu0442u00a0u043du0443u0442u0443u044e direction of flight form, with the level of t u0430u043au043eu0433u043e u043du043eu0441u0438u0442u0435u043bu00a0, having a ring shape are in tandem.;9. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that the u0434u043bu00a0 u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 heavy missile launchers are classical and u0437u0430u043au0440u0435u043fu043bu00a0u044eu0442 in the central part of the u0442u043eu0440u043eu0438u0434u0430u043bu044cu043du043eu0439 warm u0432u043du043eu0439 containers with airtight u043eu0431u043eu043bu043eu0447u0435u0447u043du043eu0439 constructs an additional static producing.;10. method for p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 so that, with a view to the heating up of the shell is hydrogen gas, the fuel u0434u043bu00a0 u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 speed u0438u0441u0442u0435u0447u0435u043du0438u00a0 through u0438u0441u043fu043eu043bu044cu0437u043eu0432u0430u043du0438u00a0 temperature heating nozzle rocket u0434u0432u0438u0433u0430u0442u0435u043bu00a0, u0434u043bu00a0 expiring in the nozzle of the nozzle liquid or gaseous hydrogen is u00a0u0434u0435 u0440u043du043eu0433u043e missile u0434u0432u0438u0433u0430u0442u0435u043bu00a0 and u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 simultaneous workthere is an additional heat from the nozzle u043eu0442u044au0435u043c missile u0434u0432u0438u0433u0430u0442u0435u043bu00a0 (is it cooling).;11. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 p.10, so that the center of gravity u0434u043bu00a0 u0441u043eu0437u0434u0430u043du0438u00a0 u0440u0430u043au0435u0442u043eu0441u0442u0430u0442u0430 fuel placed in front of the u0434u0438u0440u0438u0436u0430u0431u043bu00a0 or an aerodynamic shape upwards, and the missile u0434u0432u0438u0433u0430u0442u0435u043bu00a0 placed in the tail part, and provide the condition u0441u043cu0435u0449u0435u043du0438u00a0 centre forward from the center of mass u0440u0430u043au0435u0442u043eu0441u0442u0430u0442u0430 u0434u0430u0432u043bu0435u043du0438u00a0 (steam u0443u0441u043du043eu0441u0442u0438).;12. device for p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0, u0433u0438u043fu0435u0440u0437u0432u0443u043au043eu0432u043eu0439 u0440u0430u043au0435u0442u043eu0441u0442u0430u0442 flat design u0434u0438u0441u043au043eu043eu0431u0440u0430u0437u043du043eu0439 or triangular form, and it has two surfaces, the upper and lower , a flat or u0434u0432u043eu00a0u043au043eu0432u044bu043fu0443u043au043bu043eu0439 form, with the u0440u0430u0437u043du043eu0441u00a0u0442 from each other at the u0440u0430u0441u0441u0442u043eu00a0u043du0438u0435, much less than their geometrical dimensions in plan and u043au0440u0435u043fu00a0u0442 to same u0441u0442u043au043eu043cu0443 u0441u0438u043bu043eu0432u043eu043cu0443 spatial frame.in this framework u043du0430u0445u043eu0434u0438u0442u0441u00a0 between casings in the u043cu0435u0436u043eu0431u043eu043bu043eu0447u0435u0447u043du043eu043c space and air jet or rocket engines u043au0440u0435u043fu00a0u0442 to frame and polo ism. u043cu0435u0436u043eu0431u043eu043bu043eu0447u0435u0447u043du043eu0433u043e space u0437u0430u043fu043eu043bu043du00a0u044eu0442 gas lighter than air, helium, hydrogen, heated air)in addition, with the use of a gas generating static producing air upper shell are transparent, multilayer, and the lower shell. turn black, with heated gas within the membranes u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 from solar radiation u043au043eu0442u043eu0440u0430u00a0, u043fu0440u043eu043du0438u043au0430u00a0 through the transparent shell, warms the inner h u0430u0441u0442u044c lower black shellin addition the gas inside the shell u043du0430u0433u0440u0435u0432u0430u0435u0442u0441u00a0 automatically in u0432u0440u0435u043cu00a0 flight at high u0441u043au043eu0440u043eu0441u0442u00a0u0445, while inside the shell u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 u0446u0438u0440u043au0443u043bu00a0u0446u0438u044e gas u0434u043bu00a0 active u0442u0435u0440u043cu043eu0440u0435u0433u0443u043bu0438u0440u043eu0432u0430u043du0438u00a0 membranes.;13. method for p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0434u043bu00a0 u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 u0434u0430u0432u043bu0435u043du0438u00a0 hydrogen u043cu0435u0436u043eu0431u043eu043bu043eu0447u0435u0447u043du043eu043c space u0440u0430u043au0435u0442u043eu0441u0442u0430u0442u0430, to u043fu043eu0432u044bu0448u0435u043du0438u00a0 reactive u0442u00a0u0433u0438 u043eu0442u0431u0440u0430u0441u044bu0432u0430u0435u043cu043eu0433u043e u0433u0430u0437u043eu043eu0431u0440u0430u0437u043d wow hydrogen shell uniformly, pressure is uniformly u0440u0430u0441u043fu0440u0435u0434u0435u043bu00a0u044eu0442 on surface membranes, which u043fu0435u0440u0435u0434u0430u0435u0442u0441u00a0 through spatial u0440u0430u0441u0447u0430 u043au0430u0442u0435u043du0430u0440u043du0443u044e system lock or u0434u0438u0430u0444u0440u0430u0433u043c internal, mutually opposite side of the membrane.;14. method for p.1, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 however that, in order to heat up from the shell of hydrogen, its u043fu0440u043eu0433u043eu043du00a0u044eu0442 through the camera u0441u0433u043eu0440u0430u043du0438u00a0 or heat exchanger, u043du0430u0445u043eu0434u00a0u0449u0438u0439u0441u00a0 in u0444u043eu043au0430u043bu044cu043du043eu043c u043fu0440u043eu0441u0442u0440 u0430u043du0441u0442u0432u0435 parabolic or spherical concentrator solar rays with the hub shell with the shape of the mirror surface, with the u0440u0430u043au0435u0442u043e u0441u0442u0430u0442u0430 u043fu0440u043eu0438u0437u0432u043eu0434u00a0u0442 spiral.u043fu0440u043eu0435u043au0446u0438u00a0 go terminator which coincides with the planet, with u0440u0430u043au0435u0442u043eu0441u0442u0430u0442, u043du0430u0445u043eu0434u00a0u0441u044c u043fu043eu0441u0442u043eu00a0u043du043du043e in sunlight, causes the load to u0442u0435u0440u043cu0438u043du0430u0442u043eu0440u043du0443u044e orbit.;15. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that the lower surface of the plane u0440u0430u043au0435u0442u043eu0441u0442u0430u0442u0430 u0432u044bu043fu043eu043bu043du00a0u044eu0442 is folded, and the space between the u0441u043bu043eu00a0u043cu0438 u0437u0430u043fu043eu043bu043du00a0u044eu0442 liquid fuel and u043eu043au0438u0441 u043bu0438u0442u0435u043bu0435u043c u0434u043bu00a0 air jet or rocket u0434u0432u0438u0433u0430u0442u0435u043bu00a0 and u0432u044bu0441u043eu043au043eu043au0438u043fu00a0u0449u0438u0435 fuel components are in the external u0441u043bu043eu00a0u0445 surface shell.;16. method for p.4, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 because when entering the atmosphere of planets annular objects equipped with membrane casings u0437u0430u043fu043eu043bu043du00a0u044eu0449u0438u043cu0438 area inside the ring, for example u043eu0440u0431u0438u0442u0430u043bu044cu043du044b e ring station with artificial gravity does not stop its rotation and u0432u0445u043eu0434u00a0u0442 in atmosphere of planets with rotation, giving rise to u043du0430u0431u0435u0433u0430u044eu0449u0435u043cu0443 on u0433u0438u0440u043eu0441u0442u0430u0431u0438u043bu0438u0437u0430u0446u0438u044e current, u0441u043eu0431u043bu044eu0434u0430u00a0 ballistic angle door and lift to drag ratio.;17. method for u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0 1, so that, with a view to u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 additional horizontal speed at a static flat u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0u043c rise in the atmosphere u043au043eu043du0441u0442u0440 u0443u043au0446u0438u0438 attach an angle alpha to the direction u043du0430u0431u0435u0433u0430u044eu0449u0435u0433u043e vertical flow and horizontal force by the use u0434u043bu00a0 horizontal p v u0435u0440u0435u043cu0435u0449u0435u043du0438u00a0 ns.;18. device for p.u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 14, so that, to the best heat transfer in u0442u0435u043fu043bu043eu043eu0431u043cu0435u043du043du0438u043au0435, u043du0430u0445u043eu0434u00a0u0449u0438u043cu0441u00a0 in focus u0433u0435u043bu0438u043eu0442u0435u0440u043cu0438u0447u0435u0441u043au043eu0439 installation with heat exchanger in u0433u0435u043bu0438u043eu043au043eu043du0446u0435u043du0442u0440u0430u0442u043eu0440u043eu043c, u044bu043fu043eu043bu043du00a0u044eu0442 as u0432u044bu043fu0443u043au043bu043eu0432u043eu0433u043du0443u0442u043eu0439 or u0434u0432u043eu00a0u043au043eu0432u044bu043fu0443u043au043bu043eu0439 u0442u0430u0440u0435u043bu044cu0447u0430u0442u043eu0439 maximum surface area, and the body in the form of a gas or a liquid u043fu0440u043eu0433u043eu043du00a0u044eu0442 u0440u0430u0441u043fu0440u0435u0434u0435u043bu00a0u00a0 r u0430u0431u043eu0447u0435u0435 body as much surface area, for example,through the spiral channels, u043du0430u0445u043eu0434u00a0u0449u0438u0445u0441u00a0 between u043fu043eu0432u0435u0440u0445u043du043eu0441u0442u00a0u043cu0438 heat exchanger.;19. device for u043eu0442u043bu0438u0447u0430u044eu0449u0435u0435u0441u00a0 1, so that, with a view to u0441u043eu043au0440u0430u0449u0435u043du0438u00a0 square and mass u043au0438u043bu0435u0439 and u0443u0432u0435u043bu0438u0447u0435u043du0438u00a0 efficiency, u0440u0430u043au0435u0442u043eu0441u0442u0430u0442u044b and space design u0441u043du0430u0431u0436 u0430u044eu0442 u043au0438u043bu0435u0432u044bu043cu0438 vertical u0430u044du0440u043eu0434u0438u043du0430u043cu0438u0447u0435u0441u043au0438u043cu0438 u043fu043eu0432u0435u0440u0445u043du043eu0441u0442u00a0u043cu0438, u0440u0430u0441u043fu043eu043bu0430u0433u0430u0435u043cu044bu043cu0438 in the lower part.