RU207630U1 - BINARY SPACE VEHICLE FOR SEARCHING AND COLLECTING EXTRATERRESTRIAL RADIATING NANO OBJECTS IN THE ENVIRONMENT OF LIBRATION POINTS OF PLANETS INCLUDING A SOLAR SYSTEM - Google Patents

Abstract

The utility model refers to small research binary spacecraft (BSC) designed to search and collect emitting nanoscale objects of extraterrestrial origin, accumulated in cosmic dust structures located in the vicinity of libration points (Lagrange points). The spacecraft contains two cylindrical bodies, in the centers of the ends of which there are telescopic rods, on which there are four multi-vector matrix rocket engines with wavy cylindrical surfaces for scanning cloudy-dusty structures, deploying and rolling up two flexible tape substrates with placed solar cells and microcontainers for indicating radiation from Stokes shift and collection of nanoobjects using electric and magnetic fields. Self-correction of the trajectory of the search for emitting nanoobjects is carried out as the fluorescence of nanoobjects excited by a long wave in the UV range is detected using indicator microcontainers located on a second flexible tape substrate and a camera for express analysis. The assembled nanoobjects are sealed by sealing the microcontainers with sealing films and simultaneously rolling them into a roll transported to Earth for laboratory research. The technical result is the possibility of correcting the search trajectory depending on the results of an express analysis of the radiating properties of extraterrestrial nano-objects with different physical properties, collected separately using an electric and magnetic field, followed by conveyor sealing of the collected nanoobjects when scanning the vicinity of the libration points of planets entering the solar system.

Description

The utility model relates to research small-sized binary spacecraft (BSC) weighing less than 1000 grams, designed to search and collect in outer space nanoscale objects of extraterrestrial origin, the clusters of which are located in the vicinity of libration points (Lagrange points) in the form of dust cloud-like structures (for example, dust clouds of Kordylevsky in the Moon-Earth system). The purpose of the research is to carry out laboratory synthesis of similar nanoobjects with new properties that are not found on Earth on the basis of the physicochemical analysis of the collected BKA emitting nanoobjects of extraterrestrial origin.

Used in the description of the utility model, the phrase "binary spacecraft" (BSC) is understood as a spacecraft consisting of two bodies and a common reinforced flexible strip solar battery located between them, deployed by unwinding a solar battery, coiled into a roll, with the reversible movement of one hull relative to the other in opposite directions and back, carried out using multi-vector matrix rocket engines (MMRM). A flexible strip solar cell (SB) is a flexible dielectric strip substrate on which an array of interconnected thin-film solar cells is applied in combination with microcontainers for collecting nanoobjects. Libration points are points where gravitational and centrifugal accelerations acting on a body placed in the vicinity of the point are balanced, and therefore the so-called "small bodies" can accumulate there (Patent for invention RU 2691686 C1, 17.06.2019, G01N 1 / 02, B64G 4/00, Method of sampling and delivery to the Earth of cosmic dust samples from the vicinity of libration points of the Earth-Moon system and a set of means for its implementation / Tsygankov O.S.).

Nanoobjects are individual nanoparticles with a size in the range of 2-100 nanometers and systems of nanoparticles that form homogeneous or inhomogeneous multi-link structures, the size of which is less than 2000 nanometers. Depending on the size and material from which the nanoobjects were formed, they can have the properties of reacting to magnetic or electric fields, depending on the surrounding factors, change their polarity instantly or keep it constantly, pass from one physical state to another, for example, from exposure to light or X-rays. photons to convert wavelengths of electromagnetic radiation (Patent for invention RU 2723899 C1, 06/18/2020, G01Q 60/24, B82Y 35/00, scanning probe of an atomic force microscope with a detachable telecontrolled nanocomposite emitting element doped with quantum dots, upconverting and magnetic structure nanoparticles core-shell / Linkov V.A., Gusev S.I., Vishnyakov N.V., Linkov Yu.V., Linkov P.V.).

Known binary spacecraft for the search and collection of extraterrestrial objects with the properties of quantum dots in the vicinity of libration points, containing two panel-shaped bodies connected to containers, a flexible substrate with thin-film solar cells, which is made in the form of a dielectric tape with the ability to roll up, with applied information , power, high-voltage buses, collinear antenna, positional barcode tape, microcontainers, each of which contains film electrodes and rigid dielectric microsubstrates, also contains two multi-vector matrix rocket motors, two retractable telescopic rods, two linear stepping motors, three reversible stepping motor, three coils for accommodating a flexible dielectric tape substrate and a sealing self-adhesive film, a pressure electromagnet, two laser rangefinders, two CCDs, two solar sensors, a barcode sensor, two disc collectors, two controllers, two voltage stabilizers, a transceiver (Patent for utility model RU 202757 U1, 03/04/2021, B64G 1/22, В82В 1/00, a binary spacecraft for searching and collecting extraterrestrial objects with the properties of quantum dots in the vicinity of libration points / Molts V .A.).

The disadvantage of the device is the inability to correct the search trajectory depending on the results of an express analysis of the emitting properties of extraterrestrial nanoobjects with different physical properties, collected separately using an electric and magnetic field, followed by conveyor sealing of the collected nanoobjects when scanning the vicinity of the libration points of planets entering the solar system ...

The closest in technical essence is a binary spacecraft for searching and collecting extraterrestrial objects with the properties of quantum dots in the vicinity of libration points, containing two panel-shaped bodies connected to containers, a flexible substrate with thin-film solar cells, which is made in the form of a dielectric tape with the ability to roll into a roll with applied information, power, high-voltage buses, a collinear antenna, positional barcode tape, microcontainers, each of which contains film electrodes and rigid dielectric micro-substrates, also contains two multi-vector matrix rocket motors, two retractable telescopic rods, two linear stepping motor, three reversible stepper motors, three coils to accommodate flexible dielectric tape substrate and sealing film, thermocouple, two laser rangefinders, two CCDs, two solar sensors, barcode sensor, two disk currents remover, two controllers, two voltage stabilizers, a transceiver (Patent for invention RU 2744277 C1, 03/04/2021, B64G 1/22, a binary spacecraft for searching and collecting extraterrestrial objects with quantum dot properties in the vicinity of libration points / V.A. ).

The disadvantage of the device is the inability to correct the search trajectory depending on the results of an express analysis of the emitting properties of extraterrestrial nanoobjects with different physical properties, collected separately using an electric and magnetic field, followed by conveyor sealing of the collected nanoobjects when scanning the vicinity of the libration points of planets entering the solar system ...

The difference between the proposed technical solution from the above is the introduction of two cylindrical bodies, which made it possible to wind a flexible solar battery directly around the bodies without the use of additional coils. The introduction of four MMRPs with wavy cylindrical surfaces generating thrust packets with given combinations of their values and directions made it possible to carry out the reverse rotation of the two bodies in combination with their reverse movement relative to each other. This made it possible, with the help of a MMPD with wavy cylindrical surfaces, to repeatedly unfold and roll up the SB. The introduction of four disk-shaped scanning laser rangefinders operating with a horizon view of 360 °, located at the ends of the cylindrical housings, made it possible to constantly track the distance between the upper and lower ends of the housings and the angle of inclination of the symmetry axis of one hull relative to the other, as well as constantly track the distance to adjacent spacecraft. when scanning the surroundings of the libration point simultaneously by several BSCs. The introduction of flat coils connected to the power supply buses located at the bottom of the microcontainers made it possible to form an array of attractive electromagnetic fields for the collection and accumulation of the investigated emitting nanoobjects with magnetic properties. The introduction of a cylindrical thermoelement connected to a retractable U-shaped rod connected to clamping linear stepper motors connected to flat stepper motors made it possible to weld one or more microcontainers with assembled emitting nano-objects with uniform pressing of the thermoelement to the surfaces of the microcontainers to be welded with applied thermal glue. The introduction of microgranules of hot-melt glue, applied to the upper parts of the microcontainers, made it possible to make a hermetic connection of the material of the sealing film with the material of the microcontainers having different heat-resistant characteristics. The introduction of a navigation stellar camera made it possible to independently correct the scanning trajectory by the stars, prevent collisions with space objects capable of destroying the spacecraft, and photograph space objects. The introduction of a camera for express analysis makes it possible to detect the radiation of nanoobjects in the form of luminescence or fluorescence of nanoobjects and in more detail, with a smaller step, scan the area of the neighborhood with a cluster of emitting nanoobjects to collect more of them in less time. The introduction of a second flexible dielectric tape substrate made it possible to place indicator microcontainers on its shadow side for collecting emitting nanoobjects. The introduction of a strip UV filter, facing the Sun, and orderly cut under it on the second sealing film with a multitude of windows, made it possible to create a continuous source of excitation of emitting nanoobjects. The introduction of the first and second stepper motors, connected to a U-shaped rod, made it possible to rotate the camera for express analysis on the investigated indicator microcontainers and the navigational stellar camera to track the environment without turning the spacecraft using the MMRD. The introduction of the fifth stepper motor connected to a spool mounted on the lower part of the second cylindrical body makes it possible to wind and unwind the second sealing film in the opposite direction of rotation from the direction of winding onto the second housing using the MMPD of the first sealing film, and winding on the first housing is carried out in one and in the same direction, which allows the indicator microcontainers to remain all the time in the shaded area (on the back of the solar panels), which is necessary to register weak fluorescence emission. The introduction of disk solar sensors located on the first and second cylindrical bodies between the webs of the first and second sealing films made it possible to orientate solar cells simultaneously with the deployment or folding of the spacecraft.

The technical result is the possibility of correcting the search trajectory depending on the results of an express analysis of the emitting properties of extraterrestrial nano-objects with different physical properties, collected separately using an electric and magnetic field, with subsequent conveyor sealing of the collected nanoobjects when scanning the vicinity of the libration points of planets entering the solar system.

The technical result of the proposed utility model is achieved by a set of essential features, namely: a binary spacecraft for searching and collecting extraterrestrial emitting nanoobjects in the vicinity of the libration points of planets entering the solar system, containing two housings, a flexible substrate with thin-film solar cells, which is made in the form of a dielectric tapes with the ability to roll into a roll, with applied information, power, high-voltage buses, collinear antenna, positional barcode tape, microcontainers, film electrodes, rigid dielectric micro-substrates, also contains multi-vector matrix rocket motors, retractable telescopic rods, linear stepping motors, thermoelectric , sealing film, solar sensor, barcode sensor, two controllers, two voltage regulators, transceiver, four multi-vector matrix rocket motors with undulating cylindrical surfaces, four linear stepper motors, four retractable telescopic rods, four disk-shaped scanning laser rangefinders, a spool, indicator microcontainers with located in them from opposite sides under rigid dielectric substrates, two film electrodes each connected to high-voltage buses and a flat electromagnetic coil located in the middle, connected to by a power bus, a second flexible dielectric tape substrate with a barcode tape applied and one row of indicator microcontainers, connected from one edge to the first cylindrical housing, and from the opposite edge mechanically to a spool, a second sealing film with orderly cut along the length of the windows with a shape repeating the shape rigid dielectric microsubstrates and with a pitch equal to the pitch placed on the second flexible dielectric substrate of the indicator microcontainers, a strip UV filter superimposed on the windows of the second sealing film, a camera for express analysis, on navigational star chamber, first, second, third, fourth, fifth flat stepper motors, first and second clamping linear stepper motors, cylindrical thermoelement, U-shaped rod, retractable U-shaped rod, microgranules of hot melt glue applied to the edges of microcontainers, the first and second housings are made cylindrical at their ends, the first, second, third, fourth disc-shaped scanning laser rangefinders are fixed, at the ends of which stators of the first, second, third, fourth flat stepping motors are located, the rotating rotors of the first and second are connected to a U-shaped rod, and the rotors of the third and fourth are connected to the first and second clamping linear stepper motors through the central through holes of the first, second, third, fourth flat stepping motors extendable telescopic rods connected to multi-vector matrix rocket motors with wavy cylindrical surfaces and, connected to the cylindrical bodies, to the side walls of which the edges of the first sealing film applied from the shadow side to the canvas of the first flexible dielectric tape substrate with microcontainers arranged in three rows are mechanically attached, the electrically conductive power buses are connected to thin-film solar cells and flat electromagnetic coils located under rigid dielectric micro substrates in microcontainers of the central row, high-voltage buses are connected to film electrodes located in microcontainers adjacent to the central row, and the information bus connects the first and second controllers located in the first and second cylindrical cases, to the ends of the first of which through the first and second flat stepper motors controlled by the first controller, a U-shaped rod is attached with an attached camera for express analysis and a navigation star camera, and the second body through the first and second pressure lines e stepper motors controlled by the second controller is connected to a retractable U-shaped rod passing through a through hole located along the axis of symmetry of the cylindrical thermoelement for uniform pressure on the edges of microcontainers with assembled nano-objects sealed by the first and second sealing films, in addition, on the first and The first and second disk solar sensors are symmetrically fixed to the second bodies at a distance equal to the spool height, the fifth flat stepping motor is attached to the end of the second body from the inner side, which is connected to the spool put on the second cylindrical body between the second disk solar sensor and the fourth disk-shaped scanning laser rangefinder and rotating in the opposite direction from the direction of rotation of the second cylindrical body.

The essence of the utility model is illustrated in FIG. 1 and FIG. 2 which shows a binary spacecraft for searching and collecting extraterrestrial emitting nanoobjects in the vicinity of the libration points of planets entering the solar system at the time of deployment of a flexible tape SB (Fig. 1 - front view; Fig. 2 - Rear view). FIG. 3 shows a structural block diagram of a binary spacecraft for searching and collecting extraterrestrial emitting nanoobjects in the vicinity of the libration points of planets entering the solar system. FIG. 4 and FIG. 5 shows a remote element A (10: 1) (Fig. 4 is a front view, Fig. 5 is a rear view) on an enlarged scale, explaining the topology of the arrangement on the first and second flexible dielectric tape substrates of conductive buses and microcontainers for collecting and subsequent sealing of the assembled emitting nanoobjects. FIG. 6, FIG. 7 - schematically explains the stages of the deployment of the BCA. FIG. 8 - the stage of scanning the vicinity of the libration point, collecting and sealing the collected nanoobjects. FIG. 9, - stage of BCA coagulation.

A binary spacecraft for the search and collection of extraterrestrial emitting nanoobjects in the vicinity of the libration points of the planets included in the solar system contains: (Fig. 1, Fig. 2) the first 1 and the second 2 cylindrical bodies, the first 3, the second 4, the third 5, the fourth 6 MMRD with wavy cylindrical surfaces, first 7, second 8, third 9, fourth 10 linear stepper motors, first 11, second 12, third 13, fourth 14 retractable telescopic rods, first 15, second 16, third 17, fourth 18 disk-shaped scanning laser rangefinders, first 19, second 20, third 21, fourth 22, fifth 23 flat stepper motors, first 24 and second 25 clamping linear stepper motors, cylindrical thermoelement 26, retractable U-shaped rod 27, first 28 and second 29 sealing films ( Fig. 1), the first 30 and the second 31 flexible dielectric tape substrates, thin-film solar cells 32, power lines 33, data line 34, high-voltage line with a polarity 35, high-voltage bus with negative polarity 36, film electrodes 37 (Fig. 4), flat electromagnetic coils 38, rigid dielectric micro substrates 39, microcontainers 40, indicator microcontainers 41, windows 42, UV strip filter 43, positional barcode tape 44, barcode sensor 45, first 46, second 47 disk solar sensors, navigation star camera 48, camera for express analysis 49, U-shaped rod 50, first 51 and second 52 controllers, first 53 and second 54 voltage stabilizers, high-voltage power supply 55, collinear antenna 56, transceiver 57, spool 58, hot melt microbeads glue 59 (Fig. 4, Fig. 5). FIG. 3, within the boundaries of closed dotted lines, there are elements structurally located in the first 1 and second 2 cylindrical bodies, λ1, λ2, λ3, λ4 are the selected wavelengths of electromagnetic radiation in the optical range, emitted by the first 15, the second 16, the third 17, the fourth 18 disk-shaped scanned laser rangefinders. λf are the fluorescence wavelengths of the collected emitting nanoobjects.

The first flexible dielectric tape substrate 30 (Fig. 4) is reinforced with dielectric closed ordered rectangular ribs in the form of edges, forming on the surface of the flexible dielectric tape substrate 30 a plurality of rectangular, top-open planar microcontainers 40. In each microcontainer 40 located along the edges of the flexible dielectric tape substrate 30, a film electrode 37 is placed on which a rigid dielectric microsubstance 39 is applied. Rigid dielectric microsubstrates 39 are made with a width less than the radius of the cylindrical body 1 and 2 to reduce the asymmetry of the roll shape when carrying out multilayer winding. Depending on the location of the film electrodes 37 at the top or bottom of the flexible dielectric substrate 30, they are connected to high-voltage buses 35 and 36 with positive and negative polarity. When the high-voltage power supply 55 is turned on, an electric field is created, which attracts oppositely charged nanoparticles to the film electrodes 37, which are deposited without reaching them on rigid dielectric microsubstrates 39. Microcontainers 40 sort nano-objects into three classes: two - for collecting negatively and positively charged nanoobjects, one - for collecting nano-objects with magnetic properties. Indicator microcontainers 41 for increasing the concentration of nanoobjects on a rigid dielectric substrate carry out an integrated collection of all nanoobjects simultaneously. An attractive electric field is created by film electrodes 37, to which a high-voltage voltage is applied, and a magnetic field is created using flat coils 38, when current flows through which an electromagnetic field is created that attracts ferromagnetic nanoobjects. Film electrodes 37 and flat coils 38 are located under rigid dielectric substrates 39.

On the second flexible dielectric tape substrate 31, indicator microcontainers 41 are arranged in one row (Fig. 5). At the bottom of each of them, under a rigid dielectric micro-substrate 39, transparent to ultraviolet (UV) radiation, there are two film electrodes 37 connected to high-voltage buses with positive polarity 35 and negative polarity 36, in the middle there is a flat electromagnetic coil 38 connected to the power bus 33. In contrast to the first flexible dielectric tape substrate 30, on which elements for separate collection of nanoobjects are placed, the second 31 flexible dielectric tape substrate provides a maximum concentration of 39 nanoobjects with mixed properties on a rigid dielectric microsubstrate, for performing express analysis for the presence of studying properties (luminescence , fluorescence). As a source of excitation, electromagnetic radiation is used, isolated from the spectrum of sunlight, with the help of a tape UV filter 43 made in the form of a film. The alternating windows 42 located under the tape UV filter 43 (Fig. 4) are cut on the surface of the second sealing film 29 with a step equal to step of distribution of rigid dielectric micro-substrates 39 on the second 31 (Fig. 5) flexible dielectric tape substrate. Electromagnetic radiation of the UV range, passing through a light filter, a microsubstance, excites nanoobjects, which convert the initial wavelength into a wavelength with a Stokes shift in the visible wavelength range, depending on the physical and chemical properties of the materials that make up the emitting nanoobjects captured by electric or magnetic fields. The camera for express analysis 49 constantly monitors the indicator microcontainer 41 closest to it and, when detecting the presence of fluorescence of nanoobjects on the surface of the rigid dielectric microsubstance 39 (excited by UV electromagnetic wavelengths), outputs a signal to the first controller 51, which reduces the scanning step of the search trajectory, for more detailed targeted search and memorizes the number of the microcontainer, the time of occurrence of fluorescence, the stellar coordinates of the point by the barcode. Fluorescence is weak radiation, and for its fixation the camera for express analysis 49 and indicator microcontainers 41 are located on the shadow side of the BKA. The dimming strip on the rear side of the solar cells, which is crossed by the emitting nanoobjects attracted for analysis, is created by the second sealing film 29, which is made opaque with UV filter windows. Conducting a preliminary analysis for the presence of fluorescence of nanoobjects in space allows collecting more emitting nanoobjects in a shorter time interval, reducing the time of laboratory analysis using probe and fluorescence microscopy by conducting research, first of all, of those rigid dielectric microsubstances of indicator microcontainers and nearby microcontainers, where emitting nanoobjects have already been detected.

To exclude the ingress of Earth nanoparticles, planar microcontainers 40 and 41 are sealed from above with the first 28 and second 29 sealing films in space and layer by layer, together with the first 30 and second 31 flexible dielectric tape substrates are wound, respectively, on the second cylindrical body 2 and on the spool 58, rotating synchronously in the opposite direction. The first sealing film 28 in the initial position is located on the shadow side (on the back of the solar cells) of the first flexible dielectric tape substrate 30 and follows its geometric shape. The identification barcode, applied to the positioning tape 44 under each vertical row of planar microcontainers 40 and under the indicator microcontainers 41, makes it possible to determine the time of sealing the microcontainers by the code read by the barcode sensor 45, and by the camera for express analysis 49 to read the barcode under indicator microcontainer 41, in which fluorescence occurred. This makes it possible to mark clusters of collected nanoobjects, for example, in the L4 and L5 libration zones in the Earth-Moon system, for topological analysis of the distribution of emitting nanoobjects in cloud-like dust structures, and to optimally self-correct search trajectories when scanning the vicinity of libration points.

For the implementation of the utility model can be used, for example, known technologies for the manufacture of components. As a multi-vector matrix rocket engine (MMRM) with a wavy cylindrical surface, a multi-vector matrix rocket propulsion system with digital control of the magnitude and direction of thrust can be used, which consists of a flat disc-shaped monolithic heat-resistant dielectric substrate with a square matrix reversible structure placed on it motor cells connected to a cylindrical hollow repeating its contour with a wavy profile by a monolithic heat-resistant dielectric substrate with a radial fan-shaped orientation of all longitudinal axes of conical micropores to the centers of alternating conjugate concave and convex semicircles, which together form a closed wavy outer surface. All cone-shaped micropores are filled with solid fuel and are ranked by volume in proportions of sequential powers of two (1-2-4-8-16-32), providing the generation of many multidirectional thrust vectors with precision digital control in binary code by the magnitude of the thrust of each cell (Patent for invention RU 2707474 C1, 11/26/2019, F02K 9/95, B64G 1/40, multi-vector matrix rocket propulsion system with digital control of the magnitude and direction of thrust of propulsion cells for small spacecraft / V.A. Linkov, S.I. Gusev, Kolesnikov S.V., Linkov Yu.V., Linkov P.V., Taganov A.I.).

In the manufacture of SBs, well-known technologies for the manufacture of flexible solar thin-film batteries made on the basis of a flexible substrate with deposited thin-film photovoltaic cells made of at least amorphous silicon (a-Si), cadmium telluride (CdTe), gallium arsenide (GaAs ) (Patent US 9758260 B2, Sep.12, 2017, B64G 1/22, B64G 1/10, LOW VOLUME MICRO SATELLITE WITH ELEXIBLE WINDED PANELS EXPANDABLE AFTER LAUNCH).

The device works as follows: after the delivery of the BCA to the libration point, the first 7, the second 8, the third 9, the fourth 10 linear stepper motors are switched on, which advance the first 11, the second 12, the third 13, the fourth 14 telescopic rods, withdrawing the first 3, the second 4, the third 5, the fourth 6 MMRD with a wavy cylindrical surface from the ends of the first 1 and second 2 cylindrical bodies. The first 24 and the second 25 clamping linear stepper motors remove the cylindrical thermoelement 26 from the cylindrical body 2 (Fig. 6). At the same time, the first 15, second 16, third 17, fourth 18 disk-shaped scanning laser range finders are turned on, operating at the selected wavelengths λ1, λ2, λ3, λ4 to eliminate the influence of interference from active or passive sources. After checking the operability of the first 15, second 16, third 17, fourth 18 disk-shaped scanning laser rangefinders, the first 3, second 4, third 5, fourth 6 MMRDs with wavy cylindrical surfaces that create rotation of the first 1 and second 2 cylindrical bodies, unwinding rolled into roll the first 30 and second 31 flexible dielectric tape substrates, while simultaneously removing one cylindrical body from the other, stretching the webs of the first 30 and second 31 flexible tape substrates in opposite directions to avoid sagging (Fig. 7). After deployment to the required length (Fig. 8) of the first 30 flexible dielectric tape substrate with thin-film solar cells 32 BKA switches to the orientation and tracking the Sun mode. The rotation of the front side of the first 30 flexible dielectric tape substrate in the direction of the Sun and its simultaneous optimal tension is carried out using the first 3, second 4, third 5, fourth 6 MMRDs with wavy cylindrical surfaces that bring closer or remove, or change the angle of inclination, respectively, of the first 1 or second 2 cylindrical bodies. Using the navigation star camera 48, the starting point of scanning is determined and the scanning trajectory of the studied vicinity of the libration currents is corrected. According to the code of the coordinates of the Sun received from the first 46 and second 47 disk solar sensors and information from the first 15, third 17 and second 16, fourth 18 disk-shaped scanning laser rangefinders about the distance and angles of the axes between the first 1 and the second 2 cylindrical bodies, are carried out synchronous angular rotations of the first 1 and second 2 cylindrical bodies, without changing the distance between them (Fig. 7). The rotation of the navigation star camera 48 or the camera for express analysis 49, fixed on the U-shaped rod 50 and connected at both ends with the first 19 and the second 20 flat stepper motors, is carried out by their synchronous rotation at a given angle in the navigation mode or the analysis mode of the caught into indicator microcontainers of 41 nanoobjects for the presence of fluorescence. On the first flexible dielectric tape substrate 30, in addition to thin-film solar cells 32 and the power buses 33 connecting them, a collinear antenna 56 and a wired bi-directional communication channel in the form of a data bus 34 are also applied to exchange information between the first 51 and the second 52 controllers.

To draw in dusty structures consisting of nano-objects, high-voltage buses 35 and 36 are placed on a flexible dielectric tape substrate 30, connected to film electrodes 37 (Fig. 4) located under rigid dielectric micro-substrates 39, on which oppositely charged nanoobjects are deposited, accumulated on the bottom microcontainers 40. The electric current generated by thin-film solar cells 32 is fed to flat coils 38, which create a magnetic field for pulling in (picking up) nanoobjects with magnetic properties, as well as magnetic nanoparticles in combination with neutrally charged structures (for example, ferromagnetic nanospheres, in the pores of which frozen colloidal solutions are located). The electric current generated by the thin-film solar cells 32 is also fed to the inputs of the first 53 and second 54 voltage stabilizers, which provide stabilized voltages to power the high-voltage power supply 55 and the transceiver 57, to charge the batteries of the first 51 and second 52 controllers and provide power to all sensors and engines. High-voltage voltage from the high-voltage power supply 55 is supplied to high-voltage buses with positive 35 and negative 36 polarity, located on the solar side of the first 30 and the shadow side of the second 31 flexible dielectric tape substrates to create attractive electric fields at the bottom of the microcontainers 40 and indicator microcontainers 41.

As the cloud structures are scanned, the microcontainers 40 and 41 are sequentially sealed. The collected nanoobjects are sealed as follows. The cylindrical thermoelement 26 with the help of the first 24 and second 25 clamping linear stepper motors, operating synchronously, is pressed parallel to the second cylindrical body 2, the second controller 52 switches on the heating mode of the cylindrical thermoelement 26, which through the first 28 and second 29 sealing films (the melting temperature of which is your melting temperature of hot-melt glue) heats micro-granules of hot-melt glue 59 (Fig. 4, Fig. 5), sprayed onto the upper part of the side walls of micro-containers 40 and 41. As a result of heating, micro-granules of hot-melt glue 59 melt, acquiring adhesive properties, glue the surface of micro-containers 40 and 41 with the surfaces of the first 28 and second 29 sealing films (Fig. 5). Simultaneously, the third 21 and fourth 22 flat stepping motors rotate the cylindrical thermoelement 26 around the axis of the second cylindrical body 2 at a certain angle and for a certain time interval determined by the program of the second controller 52 to seal one or more lines of microcontainers 40 and 41. After the completion of the segment sealing cycle ( segment thermal bonding using temperature and pressure) the third 21 and fourth 22 flat stepping motors move the cylindrical thermoelement 26 to its original angular position, and the first 24 and second 25 clamping linear stepper motors move the cylindrical thermoelement 26 from the second 2 cylindrical body for winding the first 30 and the second 31 flexible dielectric tape substrates and start sealing the next microcontainers 40 and 41.

FIG. 6 and FIG. 7 - schematically explains the stages of the deployment of the BCA. FIG. 8 - the stage of scanning the vicinity of the libration point, the collection and sealing of the collected nanoobjects. FIG. 9 - stage of BKA coagulation. FIG. 6, the first stage is testing rangefinders and electronic equipment. FIG. 7, the second stage is the advancement of the engines and the orientation of the spacecraft position on the Sun. FIG. 8, the third stage is the deployment of a flexible substrate with placed photocells and microcontainers for picking up extraterrestrial nanoobjects and moving the spacecraft around the libration point, as well as collecting nanoobjects by attracting them to the surfaces of rigid dielectric microsubstrates located in open microcontainers, and subsequent sealing of the open parts of the microcontainers with assembled nanomaterial, sealing with a sealing film. A schematic of a multi-layered scannable dust cloud is shown in the background. FIG. 9, the fourth stage - the complete rolling of the flexible substrate into a roll and the transition of the system to the energy-efficient standby mode of the transport spacecraft for moving the assembled nanoobjects to the research laboratory of electron and probe microscopy located on Earth or on an orbital station in space.

The proposed design of a binary spacecraft for the search and collection of extraterrestrial emitting nanoobjects in the vicinity of the libration points of planets included in the Solar System allows: to unfold and collapse a search flexible tape of a large area between two stretching shunting MMRDs with a wavy cylindrical surface. Correct the search trajectory depending on the concentration of emitting nanoobjects detected during the express analysis of the investigated dust-cloud structure with simultaneous separate collection of nanoobjects with magnetic and non-magnetic properties that fall into the zone of attraction of electric and magnetic fields. Implement conveyor sealing of nano-objects assembled on rigid micro-substrates, divided by classes and placed in appropriate micro-containers, in combination with rolling a flexible tape web into a compact, transportable roll, which previously could not be done using known designs of small-sized spacecraft.

Claims (1)

A binary spacecraft for searching and collecting extraterrestrial emitting nanoobjects in the vicinity of the libration points of planets entering the solar system, containing two housings, a flexible substrate with thin-film solar cells, which is made in the form of a dielectric tape with the ability to roll into a roll, with applied information, power, high voltage buses, collinear antenna, positional barcode tape, microcontainers, film electrodes, rigid dielectric microsubstrates, also contains multi-vector matrix rocket motors, telescopic telescopic rods, linear stepper motors, thermoelement, sealing film, solar sensor, barcode sensor controller, two voltage stabilizers, a transceiver, characterized in that it contains four multi-vector matrix rocket motors with wave-shaped cylindrical surfaces, four linear stepping motors, four telescopic rods, four re-disk-shaped scanning laser rangefinder, spool, indicator microcontainers with placed in them on opposite sides under rigid dielectric substrates, two film electrodes each connected to high-voltage buses and a flat electromagnetic coil located in the middle, connected to a power bus, a second flexible dielectric tape substrate with applied by a barcode tape and one row of indicator microcontainers, connected from one edge to the first cylindrical body, and from the opposite edge - mechanically to a spool, a second sealing film with windows arranged in orderly cut along the length with a shape that repeats the shape of rigid dielectric micro-substrates, and with a pitch equal to the pitch placed on the second flexible dielectric substrate of the indicator microcontainers, a strip UV filter superimposed on the windows of the second sealing film, a camera for express analysis, a navigation star camera, the first, second, third, fourth, fifth planes stepper motors, the first and second clamping linear stepper motors, a cylindrical thermoelement, a U-shaped rod, a retractable U-shaped rod, microgranules of hot melt glue applied to the edges of the microcontainers, the first and second bodies are made cylindrical at their ends, the first, the second , the third, fourth disk-shaped scanning laser rangefinders, at the ends of which the stators of the first, second, third, fourth flat stepping motors are located, the rotating rotors of the first and second are connected to the U-shaped rod, and the rotors of the third and fourth are connected to the first and second clamping linear stepping motors through the central through holes of the first, second, third, fourth flat stepping motors extend telescopic rods connected to multi-vector matrix rocket engines with wavy cylindrical surfaces, connected to cylindrical bodies, to the side walls of which I The edges of the first sealing film, applied from the shadow side to the canvas of the first flexible dielectric tape substrate with microcontainers placed in three rows, are mechanically attached, the electrically conductive power buses are connected to thin-film solar photocells and flat electromagnetic coils located under rigid dielectric micro-substrates in the microcontainers of the central row are connected to film electrodes located in microcontainers adjacent to the central row, and the information bus connects the first and second controllers located in the first and second cylinder-shaped bodies, to the ends of the first of which through the first and second flat stepping motors controlled by the first controller is attached P- shaped rod with attached camera for express analysis and navigation star camera, and the second body through the first and second clamping linear stepper motors controlled by the second controller is connected to the retractable nd U-shaped rod passing through a through hole located along the axis of symmetry of the cylindrical thermoelement for uniform pressure on the edges of microcontainers with assembled nanoobjects sealed by the first and second sealing films, in addition, on the first and second bodies at a distance equal to the height of the spool, symmetrically the first and second disk solar sensors are fixed, the fifth flat stepping motor is attached to the end of the second housing on the inner side, which is connected to the spool put on the second cylindrical housing between the second disk solar sensor and the fourth disk-shaped scanning laser rangefinder and rotating in the opposite direction from the direction of rotation the second cylindrical body.

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