Volume 19, Nº 4 (2018)
- Ano: 2018
- ##issue.datePublished##: 15.12.2018
- Artigos: 19
- URL: https://journals.eco-vector.com/2712-8970/issue/view/7671
Articles
NONPARAMETRIC ALGORITHMS FOR RESTORATION OF RANDOM FIELDS
Resumo
Numerous practical tasks are closely connected with the need to restore fields of one nature or another from noisy experimental data. A feature of this problem is that a priori information isn't often enough for the description of this field accurately to within a set of a vector of parameters. This is due to the fact that information can be polytypic on the various channels of multidimensional processes. It means that the information matches to various levels of a priori in- formation. In this article special attention is paid to this problem. The corresponding algorithms of identification are used in the presence of a priori information of parametric type. In the presence of a priori information of parametric type, it is advisable to use the appropriate identification algorithms when the structure of field models is defined accu- rately to within a set of parameters and their subsequent evaluation, as current information arrives. If a priori informa- tion isn't enough, it is expedient to the researcher to use nonparametric estimates of Nadaraya-Watson for restoration of the respective fields. At the same time it is essential to determine whether all the channels of the multidimensional system are N- or T-processes. N- or T-processes are processes at which entrance or output components are stochastic - dependent and this dependence is unknown in most cases. The fields of distribution of impurity of harmful substances in atmospheric air of the city are considered as an ex- ample of use of similar processes. Nonparametric assessment of function of regression is applied as an algorithm of restoration of this field.
Siberian Aerospace Journal. 2018;19(4):574-580



MATHEMATICAL MODELING OF THE COST OF SECONDARY HOUSING IN THE CITY OF KRASNOYARSK IN 2017
Resumo
In this article the authors collected and analyzed data on the cost of second housing in the city of Krasnoyarsk in 2017. The number of the objects for analysis accounted for 1609 apartments. The authors considered the quantitative characteristics of one-room, two-room, three-room and four-room apartments. The purpose of the work is to identify the factors that have a significant impact on the formation of the price of the apartment, and build a dependence of the cost of the apartment on these factors. The mathematical apparatus for the analysis of the considered dependences is correlation and regression analysis. Because of the significant spread of data, this array is divided into groups of apartments with different number of rooms. The results of statistical analysis of the obtained sets are presented in the form of frequency histograms. The indicators that affect the cost of the apartment are analyzed. It is shown that only 4 factors are essential: a floor, a total area, a living room and a kitchen. The calculation was performed using MS Excel. The main statistical characteristics for each sample were calculated in the article. On the basis of these characteristics statistical conclusions about the nature of the distribution of populations were made. The authors showed that the median for one -, two-and three-room apartment complexes is slightly less than the average value of the sample, the fashion is slightly less than the median, and there is no long tail of the distribution. And the average value reflects the ”Central value”. The distribution curve has a higher and sharper vertex than the normal distribution. For one-room and two-room apartments the difference between the average costs of one square meter is not statisti- cally significant. Therefore, in groups of one-and two-bedroom apartments average prices per square meter are ap- proximately equal. The same effect is for a pair of two-bedroom and four-bedroom apartments. In other pairs differ- ences are statistically significant. The analysis shows that the most frequently offered for sale apartments have a cost close to the average. When dividing a set of apartments into groups by the number of rooms, samples are obtained, the empirical distributions of which are close to normal and, accordingly, the construction of regression models for such sets is justified. The study confirms the high impact on the price of the apartment offered for sale, the total area and the moderate influence of other factors. The constructed models adequately describe the experimental data.
Siberian Aerospace Journal. 2018;19(4):581-588



FILLING THE GAPS IN THE INPUT AND OUTPUT DATA USING THE ALGORITHM OF NONPARAMETRIC IDENTIFICATION
Resumo
The task of identifying systems, that is, determining the structure and parameters of systems from observations, is one of the main tasks of a modern theory and technology of automatic control. The accuracy of solving the identifica- tion problem directly depends on the quality of the initial data (sample of observations). However, the data may contain various shortcomings, in particular, gaps. Gaps in the data are due to a variety of reasons, such as inability to observe, lack of necessary tools, and so on. The easiest method of working with such data is to exclude from the table an indicator (column) or an object (line) with a space. With a large number of gaps in the data, this approach leads to a reduction in the accuracy of the model due to a reduction in the sample size. It is important to note that in the described case the complexity of solving the identification problem increases, especially when the density of passes is high, their location is irregular, and the data is insufficient (very little). The aim of the paper is to improve the accuracy of solving the problem of identifying discrete-continuous multidi- mensional processes from samples of observations with gaps. To achieve this goal, methods of mathematical statistics, data analysis, and mathematical modelings were used. In the article the algorithm of a non-parametric estimation of the regression curve in a discrete-continuous process in the task of filling out the admissions of the observation matrix is described. Moreover, a model is built based on this algorithm. Two computational experiments were carried out. The first experiment was conducted in the presence of gaps in the output variable matrix of observations. The second experiment was conducted with gaps in the input variables. The experiments were conducted at different sample sizes. Based on the results of the algorithm under vari- ous conditions, conclusions are given. The results of the work can be useful in creating control systems for multidimensional discrete-continuous processes.
Siberian Aerospace Journal. 2018;19(4):589-597



3D TREE MODELING ALGORITHM
Resumo
Nowadays tree modeling algorithms are used in different fields of activity: from computer games to the plantation forest management. Tree modeling algorithm parameters can depend on different factors: it could be features of land- scape, climate or geographical location. Depending on the tasks to be solved, the detail level of the created model is chosen. Forest management tasks often do not require a high detail level, it is sufficient to construct a schematic plantation model. For computer games the creation of photorealistic models is required. The paper proposes an algorithm of 3D tree modeling which consists of the following steps: first step - building a tree framework (modeling the growth of a tree and adding new nodes), while under the framework is meant a set of three-dimensional vectors with attributive data for each vector; then building a tree and overlaying textures. The trunk and branches of the modeled tree are approximated by truncated cones, the axes of which are the vectors of the frame. The tree model constructing algorithm is iterative. Every iteration is a tree growth stage. Thus, the tree is gradually grown to the required level. The developed algorithm allows modeling trees of different state categories. The feature of the proposed algorithm is the possibility of constructing a three-dimensional tree model with any detail level. For example, for coniferous trees it is possible to built a tree up to each needle.
Siberian Aerospace Journal. 2018;19(4):598-604



MULTILEVEL EVALUATION OF QUALITY INTERACTIVE ELECTRONIC TECHNICAL MANUALS FOR AVIATION TECHNOLOGY
Resumo
The method of multi-level quality assessment of interactive electronic technical manuals (IETM) for aircraft con- tains the main approaches, methodological and logical-mathematical tools for the implementation of multiparameter evaluation of the quality of electronic content of these manuals. The paper postulated that the goal of assessing the quality of IETM for aviation equipment is to obtain a consolidated conclusion on the degree of satisfaction of the need to create interactive electronic technical manuals in the conditions of vagueness of the initial expert data used for evaluation. It is shown that the quality assessment of interactive electronic technical manuals for the operation and repair of aviation equipment is obviously linked to non-numeric or “soft” measurements, due to the fuzzy nature of the initial qualimetric data obtained from an expert. In this version, “measurement” should be understood as a manipulation in which some strictly ordered quality gradations correlate in accordance with the IETM for the operation and repair of aviation equipment properties. In the role of quantitative measurement results, not only real numbers are considered, but also other algebraic groups that necessarily have an order relation between their elements, that is, a similarity of the inequality relation between numbers. The multi-level quality assessment of interactive electronic technical manuals for aeronautical engineering consists of the following steps: 1. Imagery of numerical vectors of values of elementary quality indicators; 2. Calculation of ranks that determine the significance of quality indicators in their compositions based on fuzzy and (or) insufficient initial data on the compositional significance of more particular indicators in the composition of more aggregated indi- cators: 3. Calculation of elementary indicators values and ratings of importance based on numerical vectors, for the analyzed performance of IETM on the operation and repair of aircraft, the values of the integral quality indicator, as the weighted arithmetic average of mathematical similar to a particular indicators.
Siberian Aerospace Journal. 2018;19(4):605-612



METHOD OF QUALITY ANOMALIES DETECTION IN INTERACTIVE ELECTRONIC TECHNICAL MANUALS FOR AIRCRAFT MAINTENANCE AND REPAIR
Resumo
The purpose of developing a method for detecting quality anomalies of interactive electronic technical manuals (IETM) in application to aircraft maintenance and repair is an objective, purposeful interpretation of assessment of the specified quality. This method is a combination of the corresponding logical-mathematical model of such anomalies designed for subject content logic circuits (SCLC), and the algorithm of its performance in the technological process of compiling interactive electronic manuals. The IETM model of quality anomalies provides the analysis of the SCLC structure as some basic graph and regards the anomaly as a more specific graph. The specific graph is a graphical description of various partial distortions of the logic presented in the form of SCLC. Such a representation of quality anomaly of IETM for aircraft maintenance and repair - by a graph isomorphically nested in the structure of its SCLC - allows to reduce the detection of such anomalies to the mathematico-algorithmic problem of detection or search for the corresponding isomorphic subgraph in the configuration of the corresponding logic circuit. This allows to detect persistable structural embeddings charac- terizing logical errors in the feeding of electronic content to IETM for aircraft maintenance and repair from the list / database of predetermined anomalous logic substructures. The proposed method for detecting IETM quality anomalies in application to aircraft maintenance and repair is both a methodological toolkit and an extensive basis for design of suitable software models for automatic procedures of valid structure and content correction in concrete interactive electronic technical manuals.
Siberian Aerospace Journal. 2018;19(4):613-621



CELLS WHOLENESS INSPECTION FOR SOLAR ARRAY USED ON PERSPECTIVE SPACECRAFTS
Resumo
New types of primary power supply have been used for wide application in Electric Power Systems (EPS) of space- crafts (S/C) recently. These are Solar arrays (SA) based on three-stage GaAs cells instead of Si cells. GaAs cells specific data is their low thickness and fragility. Due to that they have low resistance to mechanical stress and crack. Cracks in cells cause their power decrease and SA power decrease in whole. At the present time SA maintenance is carried out by the following methods: the visual method of cells wholeness in- spection (to detect cells and protective glass wholeness), SA current-voltage characteristic measurement, and the elec- tro-luminescence method. These methods do not allow detecting defects reliably and safely like hidden cracks in cells. It is necessary to define the method which will help to detect a defective cell without direct SA connection. It means a non-contact method. The content of the proposed method consists in cells illumination by lasing with wave length (0.40-0.55) µm (the green spectrum domain). It produces luminescence and the cell reflects light in the red spectrum domain. The experiment of automatic visual SA cells inspection has been performed on the test stand at JSC “ISS”. This stand has the moving platform which can be moved along SA as in vertical and also horizontal directions. On the plat- form there is a camera and laser producing light in the green spectrum domain. When the platform is set opposite the tested cell, laser is switched on and its beam is pointed at the cell. Lumines- cence appears in lasing and the cell surface reflects the light in the red spectrum domain. The camera registers the emission to measure the cell luminescence spectrum intensity by means of software (S/W). Then this value is compared by S/W with luminescence spectrum intensity value received and recorded in PC mem- ory before the cell- etalon testing. This test stand based on the electro-luminescence method allows us to define cells defects presence without contact and hidden cracks; to decrease impact of human factor.
Siberian Aerospace Journal. 2018;19(4):624-630



MODELING COMPONENTS OF BIOREGENERATIVE LIFE SUPPORT SYSTEM INTENDED FOR SPACE PURPOSES
Resumo
We have developed a linear model for compiling and optimizing food components in a bioregenerative life-support system (BLSS) intended for space purposes in the Excel environment using OpenSolver public add-in with COIN-OR- CBC solver. The independent variables in the model are the masses of ingredients used in dishes. The objective functions of modeling are to minimize the total mass of the daily diet and maximize its antioxidant potential. The daily intakes of nutrients in the menu are limited to NASA standards. The upper and lower limits are also imposed on independent variables and the masses of dishes. We have found the content of nutrients in ingredients in open databases. The menu includes the first course, the second course, snacks, desserts, drinks, bread and water. We have presented an example of a concrete calculation of the daily menu consisting of 12 dishes: fresh-soup, chicken with rice, the roast, sausages, tofu, chickpeas, candied nuts, bread, goat milk, soy milk, cocktail and water. These dishes are prepared using 24 ingre- dients: table salt, water, wheat grains, rice, quinoa, millet, sweet potato, white potato, carrots, safflower oil, soybeans, chickpeas, lentils, cowpeas, strawberries, tomatoes, onions, garlic, chili pepper, quail, pork, tilapia, goat’s milk and sugar. The ingredients being used represent edible biomass of plants and animals that are candidates for inclusion in BLSS. Caloric content of a daily diet is assumed to be equal to 2800 kcal. It is shown that food imbalances in the esti- mated daily menu are caused by a shortage of estimated daily intake of pantothenic acid, and also by an excess of iron, phosphorus and saturated fats. Excess intake of iron and phosphorus may not be critical for the health of the users of BLSS. The minimum weight of the daily menu is 2641 g, and its antioxidant potential can reach 14 mmol Ttrolox- equivalent.
Siberian Aerospace Journal. 2018;19(4):631-636



THE ANALYSIS OF THE IMPACT OF THE METHOD OF FASTENING ON STRAIN-STRESS BEHAVIOR OF COMPOSITE OVERWRAPPED PRESSURE VESSEL
Resumo
Currently, composite overwrapped pressure vessels (COPV), with high weight efficiency, are widely used in spacecraft (SC). In satellite construction COPVs provide necessary volume of working fluid for the realization of a highly efficient scheme of raising SC into geostationary orbit using standard electric propulsion engines. The issue of using such vessels in order to increase the period of active lifetime of SC and the implementation of deep-space exploration programs is relevant as well. The urgent task is to ensure the reliability of COPVs. The study of foreign literature suggests that fastening elements in direct contact with the vessel, have an important impact on the strain-stress behavior (SSB) of the vessel. The paper discusses the basic methods of fastening large-sized COPVs having a spherical shape - an adapter module is made in the form of a “skirt” and a cable-stayed system. We have created a finite element model (FEM) of COPV to analyze the effect of fastening elements on SSB of COPV. The analysis of the obtained results of the calculation shows that a cable-stayed system has almost no effect on SSB of COPV, in contrast to a composite “skirt”, which reduces the effective stresses in the place of attachment to the vessel by two times or more, causing uneven distribution of stresses. The composite “skirt” directly transfers its buckling mode to the vessel, which reflects the significant effect of the “skirt” on the vessel’s SSB. The use of a composite “skirt” in comparison with a cable-stayed system has high probability of COPV failure. The obtained results show that a cable-stayed system is more effective way to fasten COPV than a composite “skirt”.
Siberian Aerospace Journal. 2018;19(4):637-643



IMPROVEMENT OF THE METHOD OF DETERMINING CAVITATION CHARACTERISTICS OF THE CENTRIFUGAL PUMPS
Resumo
Cavitation is a process of formation of vapor bubbles within a liquid at low pressure regions. There are strain ten- sions at low-pressure region, which lead to a gap, producing cavitational cavities. These cavities contain vapor bub- bles. When cavities come to a high pressure region, they collapse, leading to a local water hammer which is able to erode the surface of a centrifugal pump. The occurring and the evolution of cavitation in liquids bound to the existence of so called cavitational cores. A physically pure liquid can resist to a strain tension efficiently, however industrial liq- uids always have cavitational cores. The cavitational cores are undissolved gas inclusions. The acceleration of evolu- tion of cavitation depends on free and dissolved gases and thermodynamic properties of liquid as well. Cavitation brings three negative factors to the performance of a centrifugal pump: performance failure - an abrupt decreasing of main parameters; erosion corrosion; low-frequency pulsations that cause the unstable work. Every centrifugal pump goes through cavitational tests for the determination of the cavitation performance. How- ever, the contemporary test methods do not have the required accuracy; moreover, the duration of a test is bigger than the work time of a pump in a rocket engine. The paper has the suggestion of the accelerated method of cavitational tests. To get the results, the new method works without maintaining of the mass flow rate, but with increased pressure-change speed on the pump entrance. For the decreasing of the error, the new method includes automatic measuring system. The authors have determined that the accelerated method with automatic measuring system does not influence the accuracy, but in the same time makes the test process shorter in time and easier to accomplish.
Siberian Aerospace Journal. 2018;19(4):644-650



METHOD FOR CALCULATING THE ENERGY CHARACTERISTICS AND SOLAR BATTERY PARAMETERS OF HIGH-VOLTAGE POWER SUPPLY SYSTEMS
Resumo
One of the main tasks arising in power supply systems (PSS) of spacecraft (SC) design is the determination of ra- tional structure in terms of providing consumers with electricity of the required quality. At the same time, a reasonable consumption of power generated by solar batteries (SB) and accumulator batteries (AB) should be realized in PSS. The choice of the PSS structure is based on the calculation and comparative analysis of PSS options, taking into account the adopted system performance criteria, the main ones being the energy and weight-dimension characteristics. For this purpose, the process of energy flows distribution in the PSS by forming a mathematical description of the PSS operating modes is carried out. In order to obtain the graphs of the SB generated power and to calculate SB parameters during the service life, a mathematical model of the SB based on the use of initial and experimental parameters of its photo- voltaic elements of any area was developed. The SB model provides the required accuracy of I-V and V-W characteris- tics calculation for any given values of illumination and temperature. In the article the method for calculating the energy characteristics of PSS and SB parameters taking into account the possibility of its limitation at the maximum or minimum level was described. It is shown that the method allows to determine the ways of rational redistribution of energy flows in the systems being designed to improve its weight- dimension characteristics by reducing the maximum design power of energy-converting equipment (ECE), which is achieved by forming a rational logic for applying the SB maximum power point tracking mode, in particular, when the spacecraft leaves the Earth's shadow. Energy balance in PSS is provided by applying correction coefficients. The calcu- lation results obtained by the method are the basis for requirements for ECE and SB design in PSS and can be used by developers and manufacturers of onboard and ground PSS.
Siberian Aerospace Journal. 2018;19(4):651-657



TRANSPARENT HEATERS BASED ON THE COPPER MICROMESH PASSIVATED BY GRAF(PH)ENE OXIDE
Resumo
The paper presents the results of creating and researching the transparent heaters with enhanced performance characteristics. The heaters are based on a composite coating of a new type by contrast with classical solutions based on transparent conductive oxide films. Such a composite coating is copper micromesh obtained using a self-organized template, stabilized by a thin film of graphene oxide (GO). The micromesh coating is formed by magnetron sputtering of copper onto a template obtained as a result of self-organized cracking of a silica film. Then, a graphene oxide film protecting the micromesh coating from thermal and chemical degradation is applied to the micromesh coating by the spray-method. A composite coating with the surface resistance of 8.9 Ohm/sq is obtained with the transparency of 82.8 % at the wavelength of 550 nm. High uniformity of heating and stability of the composite coating are shown when operating under heating up to 97.2 °C for a long time (24 hours). The composite coating of the GO / Cu micro- mesh on a glass substrate 2 mm thick is characterized by the thermal resistance value of 134.2 °C·cm2·W-1, while the ITO literature sample on an equivalent substrate is characterized by the thermal resistance of 94.04 °C·cm2·W-1, which indicates higher heating efficiency at the same specific power dissipation. This fact opens up prospects for its use as an anti-icing coating in aerospace industry.
Siberian Aerospace Journal. 2018;19(4):660-667



IMPROVEMENT OF THE METHOD OF CALCULATING THE UNIVERSAL JOINTS TRANSMISSION ANGLE WITH THE USE OF THEORETICAL AND EXPERIMENTAL STUDIES
Resumo
A technique for improving the calculation of the angle of twisting of a universal joint shaft. The design of the stand for testing universal joint gears is proposed, which includes an electric motor whose output shaft is connected to the input shaft by a mechanical gearbox connected by an output shaft to an input shaft tested by cardan gear mounted on the frame. The output shaft of the universal joint gear is connected to the input shaft of the gear reducer mounted on the additional frame together with a loading device which is hydraulic and is a hydraulic pump whose shaft is connected to the output shaft of the dispensing gear. The input channel of the hydraulic pump is connected to the hydraulic tank with the working fluid, and its output channel is connected to the input channel of the throttle, which regulates the load. Be- tween the throttle and the hydraulic pump is installed a pressure gauge calibrated in units of braking torque and a safety valve for discharging excess pressure into the hydraulic tank. The output channel of the throttle is connected to the hydraulic tank through the heat exchanger. The safety valve is electrically connected to an electrocontact manome- ter that is connected to the electrical network and is a DC solenoid valve. The results of the tests of universal joints gears in four modes of operation, characterized by varying values of the torque and braking moment and changing the design parameters of the universal joints transmission in each experiment. The equation of linear regression depend- ence of the twist angle of the universal joints shaft on the factors: the length of the universal joints gear; angle of kink in universal joints transmission; electric motor power; engine speed; braking force from the hydraulic fluid pressure. The boundaries of the confidence intervals of the angles of twisting of the universal joints transmission are found. The reli- ability and adequacy of the results of theoretical studies is confirmed by experimental studies carried out at the stand with similar theoretical data.
Siberian Aerospace Journal. 2018;19(4):668-676



MATHEMATICAL MODEL OF CONDUCTING NANOPORE FOR MOLECULAR DYNAMICS SIMULATIONS
Resumo
An electrostatic model of conducting nanopore is presented in the paper. The model does not require solution of the Poisson equation for the potential. This model is intended for use in simulation of transport phenomena of charged par- ticles in conducting nanopores by the method of molecular dynamics. This method is based on Newton’s equations of motion and it allows one to determine the variation of position, velocity and acceleration of particles with time. The electric field from the charge distributed over the nanopore surface is approximated by the field from fictitious point charges on the same surface. To verify the proposed model of fictitious charges system capacitance is calculated. The obtained values of capacitance are compared with classical results for conducting tubule and with the results obtained by the other similar method. The comparison shows that relative discrepancy between results is less than 10 %. There is a need to further develop the proposed model both in case of a large number of fictitious charges and in case when charged particles are in close proximity to the nanopore surface. The proposed method can be easily applied to an ar- bitrary shape nanopore. The model can be used in the development of various nanodevices, among them the devices used in life support systems of manned space vehicles.
Siberian Aerospace Journal. 2018;19(4):677-682



TECHNOLOGICAL EQUIPMENT ANALYSIS OF AUTOMATED MONITORING SYSTEMS OF FLUE GASES AT POWER PLANTS
Resumo
Nowadays one of the priorities of Energy Strategy of Russia is to organize constantly operating systems of continuous industrial monitoring of harmful emission out of coal-fired power plants into the atmosphere. The given paper considers the equipment for production and environmental monitoring of home developers and manufacturers, operated at some power plants of the Russian Federation at the lower level of monitoring of gas emission. At this level, measurements on the basis of agreed and certified methods, gathering and conversion of primary information to a standard form, routine maintenance and monitoring of the functioning of measuring systems and auxiliary equipment are carried out. Various gas analyzers and gas sections can be used to determine the composition of the combustion products in organization continuous monitoring at power plants. The selection of specific gas analytical systems is associated with certain difficulties, since they all have their advantages and disadvantages. Moreover, it is necessary to take into account a lot of different factors and parameters for the optimal selection of the equipment. The task of gas analytical systems selection is multicriterial. Difficulties in solving this problem are caused by the fact that the criteria may contradict each other (for example, high technical capabilities may complicate the operation of the system and increase its cost) and they may not be quantified. The selection of gas analytical systems for production and environmental monitoring should be as objective as possible, independent of the preferences of individual experts and specialists. The presented description of the equipment for production and environmental monitoring allows for an expert comparison of the technical characteristics of gas analyzers. Based on the methods of substantiating decisions on the selection of the structure of equipment in innovative projects, conclusions are drawn from the results of the analysis performed on 11 expert- relevant parameters.The recent expert analysis can supplement the results of the preliminary survey by the personnel of the power plant or a at power plants applied for the development of the technical specifications. It is recommended to carry out a feasibility investigation in decision making, taking into account the features of the equipment, production conditions, safety requirements and serviceability.
Siberian Aerospace Journal. 2018;19(4):683-690



AUTOMATIC CONTROL SYSTEM OF O2 AND H2 CONCENTRATIONS IN TECHNOLOGICAL GAS CIRCUITS OF BTLSS SPACE APPLICATION
Resumo
The Institute of Biophysics SB RAS is developing a physical experimental model of a closed ecosystem (EMCS) simulating mass-exchange flows in the presence of a calculated proportion of human metabolism. The model is de- signed to check the compatibility of the higher plant link with the biological and physicochemical links in the process- ing of organic wastes that are being developed. In this connection, the EMCS does not contain a number of auxiliary reactors (decomposition of urea, nitrification of ammonia and synthesis of hydrogen peroxide), the direct interaction of which with the plant link is either excluded, or do not have a negative impact on cultivated plants. The absence of these reactors leads to an imbalance in the flow of substances in the system; in particular, excess oxygen is formed as a result of the process of “wet combustion” of organic wastes in hydrogen peroxide. To compensate for the model gas balance, a special gas circuit is developed in which oxygen is removed by binding to hydrogen obtained by electrolysis of off- system water. To control this process, an automatic gas concentration monitoring system has been developed that allows maintaining the concentration of hydrogen in a safe range without an operator's presence, stopping the process by achieving the required oxygen concentration, and also recording the sensor readings into the database for further processing. In addition to the proposed methodological approach, the developed control system can be used in full- scale biotechnical life-support systems to monitor the oxygen / hydrogen composition of a gas medium in a gas circuit of other physicochemical processes, for example, in the synthesis of hydrogen peroxide and ammonia nitrification.
Siberian Aerospace Journal. 2018;19(4):691-697



FEATURES OF SYNTHESIS OF COMPOSITE MATERIAL BASED ON SILICON DIOXIDE AND CARBON NANOTUBES
Resumo
Today, there are many papers showing the effectiveness of the use of carbon nanotubes as additives to composites. Their use in polymers is especially successful, but the efficiency of their use in ceramics poses many questions. The aim of the work was to study the effect of the addition of carbon nanotubes on the properties of ceramics. For this purpose, pure silica, obtained by the hydrolysis of tetraethoxysilane in an alkaline medium, was taken as a model. The obtained granules of the material were well sintered at 900 ° C and it was decided to compound this material with carbon nano- tubes. Depending on the method of introducing, the result turned out to be diametrically opposite. Nanotubes intro- duced during the synthesis of silica played a role in the formation of silicon dioxide grains and effectively compacted the material, increasing its hardness. On the contrary, nanotubes grown in ceramic pores wedged the grain of silicon dioxide, making the material softer. In the first case, it is important to note that the synthesis of ceramics is not affected by the synthesis of nanotubes. In turn, nanotubes always affect the process of forming ceramics. This influence leads to a change in the structure of the grains of ceramics, and as a consequence of the mechanism of interaction between them, which in turn changes the density and strength of the ceramics. In the second case, in order to grow nanotubes in the pores and cavities of the ceramic material, one must first im- pregnate the ceramic material with a catalyst. Thus, there is a requirement for a precursor of the catalyst - the absence of its interaction with ceramics. The second requirement is for inertness of the ceramics, both to the catalyst and to the entire synthesis process. In addition, it is necessary that the structure of the pores does not change during the synthesis, i.e. they did not close during the synthesis of nanotubes, but provided transportation of the starting materials and reac- tion products. Therefore two mechanisms that affect the formation of a composite ceramic material have been described. The described composite can be used in the rocket and space industry for compounding ceramic fairings and thermal insu- lation.
Siberian Aerospace Journal. 2018;19(4):698-702



PROSPECTS FOR THE DEVELOPMENT OF THE SYSTEM OF BENDING PIPELINES OF 3D CONFIGURATION IN PRODUCTION
Resumo
The paper presents a general description of the production process of pipelines of complex configuration (TSC). Narrow directions and specializations that take a significant part in the manufacture of spatial piping systems (PTS) and fundamental technologies in this process are described on a multilateral basis. The object of the description is a base module of the upper stage (BMRB), which has both a civilian purpose - output of the payload by missiles carry- ing medium and heavy classes to a geostationary orbit, trajectories, and a special purpose. The subject of the descrip- tion is a methodology of the pipeline bending process. The article is divided into introduction, four sections describing this process and conclusion. The beginning of the article provides a rationale for the relevance of the topic under con- sideration, the strategic importance of the industry and the goal. The state need for BMRB for heavy launch vehicle “Angara-A5” for the next decade is determined. The functional assignments of the BMRB pipelines and the influence of the operating parameters of the components in the pipelines on their dimensions and material are described. The proc- ess of preparing the production technology of the pipeline is divided into nine stages: the receipt and study of design documentation (CD) in the form of 2D drawings with technical requirements and dimensions; design modeling of a part in a 3D model; definition of equipment manufacturing parts; technological preparation of the pipeline for bending; the operation of the direct manufacture of the preliminary product - the standard; measurement of the size of the resulting standard; analysis and solution of the possibility of further use of the standard; adjustment of the program of a flexible machine with numerical control (CNC) through the correction factors; assembly of the pipeline as part of a complex pipeline using a pneumatic-hydraulic scheme (CBC) with a directive technology approval. An algorithm for construct- ing a pipeline model is described; it is divided into nine main stages. Then a general description of the software module for a CNC machine and flexible pipelines are given. An international standard governing the development of a software module for CNC machines with a brief description of the sequence of preparatory and auxiliary commands is consid- ered. A block diagram of creating a control program for a pipe bending machine is shown. In conclusion, the promising directions of the development of the technology of flexible TSK are shown, in particular through the introduction of new equipment into production: universal technological interception of pipe bending; special bending head with induction function, as well as through the creation of a universal process technology of flexible TSK allowing not to resort to the creation of new technological processes for pipelines of different diameters, lengths, materials and taking into account the features of the machine .
Siberian Aerospace Journal. 2018;19(4):703-715



ENERGY RECUPERATION OF POSITIVELY CHARGED IONS
Resumo
It is important to recuperate the energy of beams of positively charged ions with simultaneous neutralization of their charge, for example, behind the nozzle of an electric rocket engine, into electric power. One of the methods to solve this problem is development and application of energy recuperators of positively charged plasma flow ions, which can be installed near the cutoff of the ERD nozzle. The process of energy recuperation of positively charged ions with simultaneous neutralization of their charge consists in electrostatic inhibition of the concentrated beam of charged particles and their interaction with the energy recuperator multicollector electrodes, which in turn are the charging electrodes of the supercapacitor. It accumulates electrostatic electricity on the elec- trodes of the supercapacitor, which can be used to power the systems of the spacecraft (SC). When positively charged ions interact with multi-collector electrodes, their charge is also neutralized by the action of the electron current com- ing from the double layer of the charging electrode of the supercapacitor. To improve the efficiency of energy recovery of positively charged ions, the volume charge of charged particles is exposed to a low-frequency electric field by an isolated control electrode installed in the cavity of a multi-collector electrode towards the moving ion flow. Development of energy recuperators of positively charged ions and increase of energy efficiency of ERD requires a scientific research based on the construction of models, principles of construction and evaluation of methods of manufacturing of their individual components.
Siberian Aerospace Journal. 2018;19(4):716-727


