This article discusses information system vulnerabilities associated with the use of personal mobile devices in financial services companies. The recommendations of this study will help to understand the importance of formulating an information security policy in this situation. The use of personal devices by employees has become commonplace in the workplace due to the increased reliance of business processes on Internet-based services and advances in technology. The organization benefits from the fact that employees buy, use their own devices, thus, the organization reduces the cost of providing employees with computer equipment and software for workplaces. However, a company can suffer huge losses if the use and connection of personal devices to the company's information technology infrastructure is not regulated and controlled. Hacking personal devices by intruders allows you to gain unauthorized access to the assets of information systems. Financial institutions handle highly sensitive information, which makes them more vulnerable when using personal devices. A qualitative research method was conducted with specially selected participants working in the information security departments of financial institutions. The study revealed the lack of an information security policy regarding personal devices and the use of an unlimited number of such devices by employees.

Keywords: personal mobile devices, information security, unauthorized access, vulnerabilities, cyber attack

Methods for determining the position of the center of gravity and the static stability margin of an aircraft in flight are considered. Based on the analysis of the motion of an aircraft as a rigid body, possible methods for determining the position of the center of gravity are determined and their errors are calculated. Comparison of the errors of various methods made it possible to conclude that it is expedient to use a method based on the use of information on the fuel reserve.

Keywords: center of gravity, moments of inertia of the aircraft, free vibrations, fuel consumption

The article is devoted to the development of numerical methods for determining the position of the center of gravity and the static stability margin of an aircraft in flight. To perform the calculations, a number of mathematical models were developed. Based on the analysis of the motion of an aircraft as a rigid body, numerical methods for determining the position of the center of gravity are synthesized and their errors are calculated. Comparison of the errors of various methods made it possible to conclude that it is expedient to use a method based on the use of information on the fuel reserve.

Keywords: simulation of the position of the center of gravity, numerical analysis of the position of the center of gravity, moments of inertia of the aircraft, free oscillations, fuel consumption.

The conclusion of the relations for the study of the propagation or diffraction of electromagnetic waves in the semiconductor layers of composite materials, which are also recommended to be used in the creation of onboard antennas and microwave devices with less weight. Both exact and simplified mathematical expressions for the rapid quantitative estimation of the complex wave number are obtained. Using the example of carbon fiber plastics with high conductivity, it is shown that their use makes it possible to create waveguide paths and antenna reflectors up to a millimeter wavelength range.

Keywords: carbon fiber, electrodynamics, composite, propagation, absorption, antenna

Theoretical relations are presented that serve to estimate the absorbing properties of thin optical films using functions that determine the envelopes of interference extrema in the transmission spectrum of a thin optical film on a plane-parallel transparent substrate, as well as the experimental results of estimating infrared losses in Ge films doped with Si.

Keywords: interference, absorption, optics, film, refractive index

In this work, the basic relations of relativistic rocket dynamics in the case of a multicomponent jet jet are obtained and investigated. Various types of relativistic rockets with a single-component jet jet are considered as special cases of the general theory. The limiting transition to nonrelativistic rocket dynamics has been made.

Keywords: relativistic dynamics, multicomponent jet stream, ion engine, photon rocket