ACTION OF A MECHANICAL INERTIAL PROPULSION FROM THE POINT OF VIEW OF THE CENTER OF MASS FOR USE IN AEROSPACE VEHICLES

Authors

  • Borys Zhurylenko State University "Kyiv Aviation Institute", Kyiv, Ukraine

DOI:

https://doi.org/10.18372/2310-5461.68.20741

Keywords:

inertial drive, center of mass, system, disks, flywheel

Abstract

Modern aviation and astronautics are based on ch

Modern aviation and astronautics are based on chemical jet engines that use the kinetic energy of a jet stream for movement in air and outer space. Currently, in addition to chemical jet engines, jet engines with high kinetic energy of a jet stream are being developed - plasma, ion, nuclear, Hall effect engines, etc. Some of them are at the research and design stage. For long flights, an engine is needed that does not require a supply of chemical fuel. An inertial engine meets these requirements. In studies of an inertial engine (N. Din 1963), when the flywheels rotate in opposite directions, the system body began to vibrate back and forth with a frequency equal to the speed of rotation of the flywheels, trembled and bounced, but the center of mass of the system remained in place. In connection with this experiment, most scientists expressed themselves quite clearly: it is impossible to build an inertial machine on a closed system. In this case, we can say that if the flywheels are rigidly connected to the body of the inertial engine, then the potential energy and momentum will be redistributed between the elements of the system, and the center of mass will remain in place. The flywheels, with their opposite ends of the mount, will have a counter-effect on the elements and the entire main mass of the system. The purpose of the work is to theoretically investigate the possibility or impossibility of creating an inertial engine that creates the movement of the center of mass of the entire system. The work theoretically investigates a system consisting of two oppositely rotating disks. The disks are located in the same plane - not at a distance of radii. The centers of rotation and the center of mass are rigidly connected to each other. The theoretical calculations performed showed that with counter-rotating disks, the moments of rotation of the system around the center of mass will be compensated along the X coordinate. Therefore, only the force acting on the center of mass in the direction of the Y coordinate will remain. Structurally, such a system can be easily implemented for an inertial propulsion system. But if we take into account the energy system that creates the force F on the disk and which is rigidly connected to the X coordinate axis, then all forces will be compensated and the inertial motion of the system will most likely not occur. It should be noted that it is unclear why in a closed system the rotational motion in one coordinate system will lead to translational motion in another coordinate system of the center of mass. To study the motion of the center of mass of the system, new experiments and theoretical calculations for other systems are necessary. emical jet engines that use the kinetic energy of a jet stream for movement in air and outer space. Currently, in addition to chemical jet engines, jet engines with high kinetic energy of a jet stream are being developed - plasma, ion, nuclear, Hall effect engines, etc. Some of them are at the research and design stage. For long flights, an engine is needed that does not require a supply of chemical fuel. An inertial engine meets these requirements. In studies of an inertial engine (N. Din 1963), when the flywheels rotate in opposite directions, the system body began to vibrate back and forth with a frequency equal to the speed of rotation of the flywheels, trembled and bounced, but the center of mass of the system remained in place. In connection with this experiment, most scientists expressed themselves quite clearly: it is impossible to build an inertial machine on a closed system. In this case, we can say that if the flywheels are rigidly connected to the body of the inertial engine, then the potential energy and momentum will be redistributed between the elements of the system, and the center of mass will remain in place. The flywheels, with their opposite ends of the mount, will have a counter-effect on the elements and the entire main mass of the system. The purpose of the work is to theoretically investigate the possibility or impossibility of creating an inertial engine that creates the movement of the center of mass of the entire system. The work theoretically investigates a system consisting of two oppositely rotating disks. The disks are located in the same plane - not at a distance of radii. The centers of rotation and the center of mass are rigidly connected to each other. The theoretical calculations performed showed that with counter-rotating disks, the moments of rotation of the system around the center of mass will be compensated along the X coordinate. Therefore, only the force acting on the center of mass in the direction of the Y coordinate will remain. Structurally, such a system can be easily implemented for an inertial propulsion system. But if we take into account the energy system that creates the force F on the disk and which is rigidly connected to the X coordinate axis, then all forces will be compensated and the inertial motion of the system will most likely not occur. It should be noted that it is unclear why in a closed system the rotational motion in one coordinate system will lead to translational motion in another coordinate system of the center of mass. To study the motion of the center of mass of the system, new experiments and theoretical calculations for other systems are necessary.

Author Biography

Borys Zhurylenko, State University "Kyiv Aviation Institute", Kyiv, Ukraine

Candidate of Physical and Mathematical Sciences, Associate Professor

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Published

2026-02-10

How to Cite

Zhurylenko, B. (2026). ACTION OF A MECHANICAL INERTIAL PROPULSION FROM THE POINT OF VIEW OF THE CENTER OF MASS FOR USE IN AEROSPACE VEHICLES. Science-Based Technologies, 68(4), 563–570. https://doi.org/10.18372/2310-5461.68.20741

Issue

Section

aviation transport