RU2761486C1 - Binary space vehicle for searching and collecting outer space objects in the neighborhood of libration points of planets included in the solar system - Google Patents

Abstract

FIELD: space technology.SUBSTANCE: invention relates to the field of space technology, and more specifically to small-sized research binary spacecraft (BSC). The BSC for searching and collecting extraterrestrial nanoobjects in the vicinity of the libration points of the planets entering the solar system contains two cylinder-shaped bodies, four multi-vector matrix rocket engines. Contains four multi-vector matrix rocket motors with undulating cylindrical surfaces, four linear stepper motors, four telescopic booms, four disk-shaped scanning laser rangefinders, a navigation star camera.EFFECT: separate collection of extraterrestrial nanoobjects with different physical properties is achieved.1 cl, 10 dwg

Description

The invention 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, 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 based on the study of materials of extraterrestrial origin collected by the BKA, their physicochemical analysis and classification, the implementation of the subsequent synthesis of such nanoparticles with known or new properties that are not found on Earth.

Used in the description of the invention, the phrase "binary spacecraft" (BSC) is understood as a spacecraft consisting of two bodies and one 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 the points where the gravitational and centrifugal accelerations acting on the body placed in the vicinity of the point are balanced, in connection with which the so-called "small bodies" can accumulate there [1].

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 nanoobjects are created, 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, convert the wavelengths of electromagnetic radiation [2].

Known micro-satellite with a solar battery, made in the form of a flexible substrate with applied thin-film solar cells, wound around the body of the micro-satellite and deployed by means of springs after entering a predetermined orbit. The micro-satellite contains: a satellite body, a deployment mechanism based on torsion springs, solar batteries made of a flexible substrate with applied thin-film photocells, motors, antennas, a solar sensor, a conical docking unit with another satellite [3].

The disadvantage of the device is the lack of the possibility of active separate collection of extraterrestrial nanoobjects with different physical properties 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.

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 motors, 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 current collectors, two troller, two voltage stabilizers, a transceiver [4].

The disadvantage of the device is the lack of the possibility of active separate collection of extraterrestrial nanoobjects with different physical properties 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 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 into a roll with applied information, power, high-voltage buses, a collinear antenna, a 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 motors, 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 disc current collectors remover, two controllers, two voltage stabilizers, a transceiver [5].

The disadvantage of the device is the lack of the possibility of active separate collection of extraterrestrial nanoobjects with different physical properties 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 the SB into a roll. The introduction of four disk-shaped scanning laser rangefinders operating with a horizon view of 360 ° degrees, located at the ends of the cylindrical bodies, made it possible to constantly track the distance between the upper and lower ends of the bodies and the angle of inclination of the axis of symmetry of one body relative to another, as well as constantly track the distance to adjacent BKA when scanning the vicinity of the libration point simultaneously by several BKA. 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 studied nano-objects 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 several microcontainers with assembled nano-objects with uniform pressing of the thermoelement to the surfaces of the welded microcontainers with applied microfluidic 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 with 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 technical result is the possibility of active separate collection of extraterrestrial nanoobjects with different physical properties 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 technical result of the proposed invention is achieved by a combination of essential features, namely: a binary spacecraft for searching and collecting extraterrestrial nanoobjects in the vicinity of 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, each of which contains film electrodes and rigid dielectric micro-substrates, also contains multi-vector matrix rocket motors, retractable telescopic rods, linear stepping motors thermocouple, sealing foil, solar sensor, barcode sensor, two controllers, two voltage regulators, transceiver, four multi-vector matrix rocket motors with wavelike cylindrical surfaces spines, four linear stepping motors, four retractable telescopic rods, four disk-shaped scanning laser rangefinders, a navigation star camera, the first and second flat stepper motors, the first and second clamping linear stepper motors, a cylindrical thermoelement, a U-shaped rod, a retractable P- a shaped rod, microgranules of hot-melt glue applied to the edges of microcontainers, the first and second bodies are made cylindrical at their ends, the first, second, third, fourth disk-shaped scanning laser range finders are fixed, at the ends of the third and fourth of which stators of the first and second flat stepping motors are located, rotating rotors of which are connected to the first and second clamping linear stepper motors, and retractable telescopic rods connected to multi-vector matrix rocket motors with wave-shaped cylindrical surfaces connected to cylindrical bodies, to the side walls of which the edges of the sealing film are mechanically attached, applied from the shadow side to the canvas of a flexible dielectric tape substrate, the electrically conductive power buses of which are connected to thin-film solar cells and flat electromagnetic coils located under rigid dielectric in micro-substrates central microcontainers, high-voltage buses are connected to film electrodes located in adjacent to the central microcontainers, and the information bus connects the first and second controllers located in the first and second cylindrical housings, to the ends of the first of which a U-shaped rod is attached with a solar sensor located in the middle and navigation star chamber, and the second body through the first and second clamping linear stepper motors, controlled by the second controller, are connected to a retractable U-shaped rod passing through with a through hole located along the axis of symmetry of a cylindrical thermoelement for uniform pressure on microcontainers sealed with a sealing film with assembled nano-objects.

The essence of the invention is illustrated in FIG. 1, which shows a binary spacecraft for searching and collecting extraterrestrial nanoobjects in the vicinity of the libration points of planets entering the solar system at the time of deployment of a flexible ribbon SB. FIG. 2 shows a block diagram of a binary spacecraft for searching and collecting extraterrestrial nanoobjects in the vicinity of the libration points of planets entering the solar system. FIG. 3 shows a remote element A (10: 1) on an enlarged scale, explaining the topology of the arrangement of thin-film solar cells on a flexible dielectric tape substrate relative to the arrangement of microcontainers for collecting and subsequent sealing of assembled nanoobjects.

FIG. 4 - The stage of removing the thermoelement from the body and transition to the initial position. FIG. 5 - The stage of pressing the cylindrical thermoelement to the sealing film and heating the microgranules of hot melt glue on the surface of the microcontainer. FIG. 6 - The stage of sealing - pressing with a cylindrical thermoelement on the area with molten hot-melt glue and moving along a given angular sector for welding a sealing film with protruding parts of one or more microcontainers.

FIG. 7, Fig. 8 - schematically explains the stages of the deployment of the BCA. FIG. 9 - the stage of scanning the vicinity of the libration point, collection and sealing of the collected nanoobjects. FIG. 10, - stage of BCA coagulation.

A binary spacecraft for searching and collecting extraterrestrial nanoobjects in the vicinity of libration points of planets entering the solar system contains: (Fig. 1, Fig. 2) first 1 and second 2 cylindrical bodies, first 3, second 4, third 5, fourth 6 MMRD with wavy cylindrical surfaces, the first 7, the second 8, the third 9, the fourth 10 linear stepping motors, the first 11, the second 12, the third 13, the fourth 14 retractable telescopic rods; first 15, second 16, third 17, fourth 18 disk-shaped scanning laser rangefinders, first 19 and second 20 flat stepper motors, first 21 and second 22 clamping linear stepper motors, cylindrical thermoelement 23, retractable U-shaped rod 24, sealing film 25 ( Fig. 1), flexible dielectric tape substrate 26, thin film solar cells 27, power lines 28, data line 29, high voltage bus with positive polarity 30, high voltage bus with negative polarity 31, film electrodes 32 (Fig. 3), flat electromagnetic coils 33, rigid dielectric micro substrates 34, microcontainers 35, positioning barcode tape 36, barcode sensor 37, solar sensor 38, navigation star camera 39, U-shaped rod 40, first 41 and second 42 controllers, first 43 and second 44 voltage stabilizers, high voltage power supply 45, collinear antenna 46, transceiver 47, microgranules of hot melt adhesive 48 (Fig. 3). FIG. 2, within the boundaries of closed dotted lines, there are elements structurally located in the first 1 and second 2 cylindrical housings, 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.

Flexible dielectric tape substrate 26 (Fig. 3) is reinforced with dielectric closed ordered rectangular ribs in the form of edges, forming on the surface of the flexible dielectric tape substrate 26 a plurality of rectangular, open top planar microcontainers 35. In each microcontainer 35 placed along the edges of the flexible dielectric tape substrate 26 placed a film electrode 32, which is superimposed on a rigid dielectric microsubstance 34. Rigid dielectric microsubstances 34 are made with a width less than the radius of the cylindrical body 1 and 2 to reduce the asymmetry of the roll shape during multilayer winding. Depending on the location of the film electrodes 34 at the top or bottom of the flexible dielectric substrate 26, they are connected to high voltage buses 30 and 31 with positive and negative polarity. When the high-voltage power source 45 is turned on, an electric field is created, which attracts oppositely charged nanoparticles to the film electrodes 32, which are deposited without reaching them on rigid dielectric microsubstrates 34. Microcontainers 35 are divided into three classes: two - for collecting negatively and positively charged nano objects, one - for collecting nano-objects with magnetic properties. An attractive electric field is created by film electrodes 32, to which a high-voltage voltage is applied, and a magnetic field is created using flat coils 33, when current flows through which an electromagnetic field is created that attracts ferromagnetic nanoobjects. Film electrodes 32 and flat coils 33 are located under rigid dielectric substrates 34.

To exclude the ingress of Earth nanoparticles, planar microcontainers 35 are sealed from above with a sealing film 25 in space and layer by layer, together with a flexible dielectric tape substrate 26 on which they are applied, are wound onto a second cylindrical body 2. The sealing film 25 is initially located on the shadow side (with the back side of solar cells) of a flexible dielectric tape substrate 26 and repeats its geometric shape. The identification barcode, applied to the positional tape 36 under each vertical row of planar microcontainers 35, makes it possible to determine the time of its sealing and from it to determine the coordinates of the trajectory intervals in which the nanoscale objects of interest were collected. 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 nanoobjects in oblong-like dusty structures during their linear or spiral scanning.

For the implementation of the invention 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 thrust value of each cell [6] ...

In the manufacture of SB, 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 ) 3].

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 21 and the second 22 clamping linear stepper motors remove the cylindrical thermoelement 23 from the cylindrical body 2 (Fig. 4). 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 disc-shaped scanning laser range finders, 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 a flexible dielectric tape substrate 26 SB, with the simultaneous removal of one cylindrical body from the other, stretching the fabric SB in opposite directions to avoid sagging (Fig. 8). After deployment to the required length (Fig. 9) of the flexible dielectric tape substrate 26 with thin-film solar photocells 27, the BKA switches to the orientation and tracking mode of the Sun. The rotation of the planes of the flexible dielectric tape substrate in the direction of the Sun and their simultaneous optimal tension is carried out using the first 3, the second 4 and the third 5, the fourth 6 MMRDs with wavy cylindrical surfaces, which bring closer or remove, or change the angle of inclination, respectively, of the first 1 or the second 2 cylindrical bodies. Using the navigation star camera 39, 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, obtained from the solar sensor 38 and information coming 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, synchronous angular rotations of the first 1 and the second 2 cylindrical bodies, without changing the distance between them (Fig. 9). On the flexible dielectric tape substrate 26, in addition to thin-film solar cells 27 and the power buses 28 connecting them, a collinear antenna 46 and a wired bi-directional communication channel in the form of a data bus 29 are applied to exchange information between the first 41 and the second 42 controllers.

To draw in dusty structures consisting of nano-objects, high-voltage buses 30 and 31 are placed on a flexible dielectric substrate 26, connected to film electrodes 32 (Fig. 3) located under rigid dielectric micro-substrates 34, on which oppositely charged nanoobjects are deposited, accumulated on the bottom of the microcontainer. 35. The electric current generated by thin-film solar cells 27 is fed to flat coils 33, 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 there are frozen colloidal solutions). The electric current generated by the thin-film solar cells 27 is also fed to the inputs of the first 43 and second 44 voltage stabilizers, which provide stabilized voltages to power the high-voltage power supply 45 and the transceiver 47, to charge the batteries of the first 41 and second 42 controllers and provide power to all sensors and engines. The high voltage from the high voltage power supply 45 is applied to high voltage buses with positive 30 and negative 31 polarity, located on a flexible substrate 26 to create attractive electric fields at the bottom of each microcontainer 35.

As the cloud structures are scanned, the microcontainers 35 are sealed sequentially. The collected nanoobjects are sealed as follows. The cylindrical thermoelement 23 with the help of the first 21 and the second 22 clamping linear stepper motors, operating synchronously, is pressed parallel to the second cylindrical body 2, the second 42 controller switches on the heating mode of the cylindrical thermoelement 23 and through the sealing film 25 (the melting temperature of which is your melting point of hot melt adhesive) heats the microgranules of hot melt glue 48 (Fig. 3), sprayed on the upper part of the side walls of the microcontainers 35. As a result of heating, the microgranules of hot melt glue 48 melt, acquiring adhesion properties, and the surface of the microcontainers 35 is glued to the surface of the sealing film 25 (Fig. 5). Simultaneously, the first 19 and second 20 flat stepping motors rotate the cylindrical thermoelement 23 around the axis of the second cylindrical body 2 by a certain angle and for a certain time interval, determined by the program of the second controller 42 to seal one or more lines of microcontainers 35. After the completion of the segment sealing cycle (segmented thermal bonding using temperature and pressure), the first 19 and second 20 flat stepper motors move the cylindrical thermoelement 23 to its original angular position, and the first 21 and second 22 clamping linear stepper motors move the cylindrical thermoelement 23 from the second 2 cylindrical body (Fig. 4) for winding flexible dielectric tape 26 and start sealing the next microcontainers 35.

FIG. 7 to FIG. 8 - schematically explains the stages of the deployment of the BCA. FIG. 9 - the stage of scanning the vicinity of the libration point, collection and sealing of the collected nanoobjects. FIG. 10 - stage of BKA coagulation. FIG. 7, the first stage is testing rangefinders and electronic equipment. FIG. 8, the second stage is the advancement of the engines and the orientation of the spacecraft position on the Sun. FIG. 9, the third stage - 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. 10, 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 at an orbital station in space.

The proposed design of a binary spacecraft for the search and collection of extraterrestrial nanoobjects in the vicinity of the libration points of planets entering the solar system makes it possible to: unfold and collapse a search flexible tape of a large area between two stretching shunting MMRDs with a wavy cylindrical surface. To carry out a combination of scanning along the search trajectory of the investigated dust-cloud structure with the simultaneous separate collection of nanoobjects with magnetic and non-magnetic properties that have fallen into the zone of attraction of electric and magnetic fields. Implement conveyor sealing of nano-objects assembled on rigid micro-substrates, divided into 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.

Sources of information

1. Patent for invention RU 2691686 C1, 06/17/2019, G01N 1/02, B64G 4/00, Method of sampling and delivery to the Earth of space dust samples from the vicinity of libration points of the Earth-Moon system and a set of tools for its implementation / Tsygankov O. WITH.

2. A patent for invention RU 2723899 C1, 18.06.2020, G01Q 60/24, 35/00 V82Υ, SCANNING PROBE atomic force microscope with a detachable remote controlled nanocomposite radiating element doped quantum dots and magnetic nanoparticles APKONVERTIRUYUSCHIMI core-shell structure / Lin'kov V. Α., Gusev S.I., Vishnyakov N.V., Linkov Yu.V., Linkov P.V.

3 Patent US 9758260 B2, Sep 12, 2017, B64G 1/22, B64G 1/10, LOW VOLUME MICRO SATELLITE WITH ELEXIBLE WINDED PANELS EXPANDABLE AFTER LAUNCH.

4. Patent for useful model RU 202757 U1, 03/04/2021, B64G 1/22, B82V 1/00, BINARY SPACE VEHICLE FOR SEARCHING AND COLLECTING OUTSIDE OBJECTS WITH QUANTUM DOT PROPERTIES IN THE NEIGHBORHOOD OF LINKOV DOTS V.A.

5. Patent for invention RU 2744277 C1, 03/04/2021, B64G 1/22, BINARY SPACE APPARATUS FOR SEARCHING AND COLLECTING OUTSIDE OBJECTS WITH THE PROPERTIES OF QUANTUM DOTS IN THE NEIGHBORHOOD OF LIBRATION POINTS / Linkov V.A.

6. Patent for invention RU 2707474 C1, 11/26/2019, F02K 9/95, B64G 1/40, MULTI-VECTOR MATRIX ROCKET PROPELLER SYSTEM WITH DIGITAL CONTROL OF VALUE AND DIRECTION OF THRUST OF MOTOR CELLS V.S. I.I., Kolesnikov S.V., Linkov Yu.V., Linkov P.V., Taganov A.I.

Claims (1)

A binary spacecraft for searching and collecting extraterrestrial 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 tires, collinear antenna, positional barcode tape, microcontainers, each of which contains film electrodes and rigid dielectric microsubstrates, also contains multi-vector matrix rocket motors, retractable 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 undulating cylindrical surfaces, four linear stepping motors, four retractable telescopic w tanges, four disk-shaped scanning laser rangefinders, a navigation star camera, the first and second flat stepping motors, the first and second clamping linear stepper motors, a cylindrical thermoelement, a U-shaped rod, a retractable U-shaped rod, microbeads of hot melt glue applied to the edges microcontainers, the first and second cases are cylindrical, at their ends are fixed the first, second, third, fourth disk-shaped scanning laser rangefinders, at the ends of the third and fourth of which are the stators of the first and second flat stepping motors, the rotating rotors of which are connected to the first and second clamping linear stepper motors, and through the central through holes of the first and second plane stepping motors extendable telescopic rods connected to multi-vector matrix rocket motors with wavy cylindrical surfaces, connected to cylindrical bodies, to to the side walls of which the edges of the sealing film are mechanically attached, applied from the shadow side to the canvas of a flexible dielectric tape substrate, the electrically conductive power buses of which are connected to thin-film solar cells and flat electromagnetic coils located under rigid dielectric micro-substrates, in central microcontainers, high-voltage buses located in adjacent to the central microcontainers, 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 a U-shaped rod with a solar sensor and a navigation star chamber located in the middle is attached, and the second body through the first and second clamping linear stepping motors controlled by the second controller are connected to a retractable U-shaped rod passing through a through hole located along the axis of symmetry of the cylindrical thermoele ment, for uniform pressure on microcontainers sealed with a sealing film with assembled nano-objects.

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