


Vol 57, No 2 (2019)
- Year: 2019
- Articles: 9
- URL: https://journals.rcsi.science/0010-9525/issue/view/9188
Article
Response of Ionospheric Total Electron Content to Convective Vortices
Abstract
The response of the total electron content (TEC) of Earth’s ionosphere to impulse geomagnetic disturbances, traveling convection vortices (TCVs), is considered in the paper. The data of networks of ground-based magnetometers in Canada and Greenland were used to reveal TCVs, whereas the TEC variations were obtained by processing the data of the IGS and UNAVCO receiving stations of the global positioning system (GPS). Ionospheric disturbances related to TCVs are detected. Using the station network makes it possible to estimate the dynamics of formation and velocity of propagation of the disturbance in space.



Water Formation in the Lunar Regolith
Abstract
This study shows that oxygen atoms can be released from a crystal lattice of silicon dioxide in the lunar regolith as parts of silver hydroxide molecules. In turn, silver hydroxide can relatively easily react with hydrogen to generate water and silver. This means that the formation of water molecules involved in near-surface lunar soil is possible. The presence of water molecules in lunar soil can affect the photoelectric properties of the lunar regolith and the parameters of the dusty plasma system over the Moon.



Flare Activity of Blazar AO 0235+164
Abstract
Data analysis of long-term multi-frequency monitoring of active galactic nucleus (AGN) AO 0235+164 in the millimeter wavelength range are presented. Using the harmonic analysis of observational data, the presence of orbital and precession periods in the binary system from supermassive black holes (SBHs) is determined: Torb ≈ 2 years and Tpr ≈ 8 years. The indicated periods are in agreement with similar periods found for other bright AGNs. In the AO 0235+164 system, other combinations of periodic components are also determined, which are possibly related to the nutation period. According to observational data of the development of flare phenomena at different frequencies, a cross-correlation analysis was performed and the shift delays of the flare times occurring at different wavelengths were determined. It was confirmed, by analogy with other AGNs, an empirical relation, to which the delays of flux variations with a frequency are obeyed having the form of the inverse logarithmic dependence. The nature of the delays can indicate the internal character of the variability of AGN emission fluxes obtained at frequencies of the centimeter and millimeter wavelength ranges. The hypothesis of jet activity of AGNs is confirmed, in which plasma formation, moving from the sources of ejection, becomes optically thin consistently on ever longer waves. Decreasing delays between frequencies for the flare in 2015 compared to the previous flare in 2008–2009 indicates a possible configuration variation in AO 0235+164 associated with decreasing in the angle between ejections and the direction to the observer.



Multicolor Photometry of a Close Binary System with an X-ray Source
Abstract
Four-color WBVR photoelectric observations of close binary system (CBS) HZ Her = Her X-1 in 1986–1994 are presented. Two-color diagrams (W–B)–(B–V) and (B–V)–(V–R) are given, which make it possible to study the behavior of the accretion disk (AD) near the main minima of binary system Min I and Min II. When constructing the light curves in all filters from the orbital phase in all phases of the precession period, the array of observations was processed considering the matrix of the X-ray source. A quantitative and qualitative interpretation of the results is given using the model of the precession of an AD of a neutron star (NS) in the direction of orbital motion of the system (direct precession). When interpreting the observational material, one of the existing models is considered, within which one can satisfactorily explain the heterogeneity of the gas flow, “hot spot,” as well as the existence of individual splashes that move along independent Keplerian trajectories around the outer parts of the NS AD of Her X-1. Using the matrix of time switching on X-ray emission of a NS and the partitioning of all series of the author’s optical observations into a specific cycle of switching on X-ray emission from a relativistic object provide a more realistic picture of CBS behavior, as well as to identify fine photometric effects occurring in it in different states.



Quaternion Equations of Disturbed Motion of an Artificial Earth Satellite
Abstract
The quaternion equations of disturbed motion of an artificial Earth satellite (AES) in Earth’s gravitational field (with regard to its zonal, tesseral, and sectorial harmonics) are obtained in four-dimensional Kustaanheimo–Stiefel variables and in modified four-dimensional variables. In the latter variables the equations of satellite motion have a simpler and more symmetric structure, as compared to the equations of motion in the Kustaanheimo–Stiefel variables. The obtained equations are linear for undisturbed Keplerian motion and, in general, have the form of equations of motion of a disturbed four-dimensional oscillator. These equations, in contrast to classical equations, are regular (they do not contain specific points of singularity) for satellite motion in the central gravitational field of Earth under an effect of disturbing forces, the description of which does not contain negative, higher-than-first powers of the satellite distance to Earth’s center. In these equations, the basic variables are Kustaanheimo–Stiefel variables, or modified four-dimensional variables proposed by the author, as well as satellite motion energy and time. The new independent variable is associated with time by the differential relation containing the satellite distance to Earth’s center of mass. The equations are convenient for applying nonlinear mechanics methods and for high-precision numerical calculations. In the case of artificial satellite motion in Earth’s gravitational field, the description of which does not take into account the tesseral and sectorial harmonics, but takes into account its zonal harmonics, the first integrals of the equations of satellite motion are found, and the replacements of variables and transformations of these equations are proposed, which allowed one to get, for studying satellite motion, closed systems of differential equations of lower dimension, in particular, the system of equations of fourth and third orders.



Mobile Space Microrobot: Concept and Application Prospects
Abstract
This paper presents a brief overview of achievements in the field of microrobotics. The tasks that can be performed by mobile microrobots in space and the corresponding requirements for design and performance characteristics of such microrobots are formulated. The concept of a mobile space microrobot with thermomechanical silicon-polyimide actuators is proposed. The basic and technological feasibility of this concept are preliminary evaluated.



The Flux Density of Particles of the Working Fluid in the Peripheral Zones of a Jet of a Magnetoplasmodynamic Thruster with an External Magnetic Field
Abstract
The results of estimated calculations of fluxes of particles of the working fluid in peripheral regions from the axial direction of the jet of a magnetoplasmodynamic (MPD) thruster with an external magnetic field with a power of 100 kW as well as the results of measurements in laboratory conditions of reverse fluxes of Li particles from the thruster are presented. Return flow measurements were conducted using the quartz microbalance method. Calculations and measurements of particle fluxes indicate that their values do not exceed ~10–8–10–7 g cm–2 s–1.



On the Rotation of a Spacecraft Carrying a Deformable Antenna in the Gravitational Field of Force
Abstract
The problem of motion, relative to the center of mass, of a satellite rotating around the center of gravity over an elliptical orbit, is studied. The satellite consists of axisymmetric solid and viscoelastic sections, with the viscoelastic section being a hemispherical antenna. It is shown that the evolution of satellite rotations can be subdivided into two stages; fast, caused by deformations under an effect of inertia forces, and slow, or the dissipative stage. It is shown that the fast evolution stage consists in the fact that the angular momentum vector is located along the satellite’s axis of symmetry (in this case, the axial moment of inertia is greater than the equatorial), and in the equatorial plane of the ellipsoid of inertia (if the equatorial moment of inertia is greater than the axial). The slow evolution stage was considered for the case where the axial moment of inertia is greater than the equatorial. It is found that slow evolution consists in decelerating the axial rotation and in the angular momentum vector inclining to the orbital plane.



Brief Communications
Formation of a Group of Small-Sized Satellites for Obtaining the Two-Dimensional Field of Ionospheric Parameters


