Verification of M.Faraday's hypothesis on the gravitational power lines - А. Т. Серков

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field. Published 21.12.2012 | By Astronomer

      2. www.sciteclibrary.ru/rus/catalog/pages/4903.html

      3. A.Serkov, Hypotheses, Moscow, Ed.LLC SIC "Uglekhimvolokno", 1998, S. 73.

      4. www.aerodriving.ru

      Chapter 2. Gravimagnetic braking of celestial bodies

Summary

      Expressed and justified the assumption that the braking satellites of the moon due to gravimagnetic forces arising at the intersection of the satellites of power lines (line tension) of the gravitational field. To calculate the forces used an equation similar electrodynamics equation of the Lorentz force. The estimated braking time for "the lunar Prospector", "Smart-1" and "Kaguya" is the same as the actual precision of ± 14 %. The scheme occurrence of gravimagnetic forces is proposed, according to which the magnitude of the force depends on Sinα, where α is the angle at which the satellite crosses the line gravimagnetic tension. For non-rotating body as Moon, this angle is equal to 90*0 and thegravimagnetic braking force has a maximum value. In the case of rotating bodies, such as Earth, the intersection of the gravimagnetic tension lines, apparently, is at a sharper angle and the braking force is substantially less (the effect of "Pioneers" and the satellites "Lageos").

      Suggested that the rotating of the central body causes the surrounding gravitational field with a periodic alternation of layers with a predominant radial and concentric orientation of the force lines of the gravitational field, which leads to a different intensity of the forces and gravimagnetic braking along the radius and emergence (allowed, elite) and unstable orbits (unresolved) orbits with high speed braking.

      The equation is proposed which determines the distance to stable orbits. In the equation a constant C = 2,48.10*8 cm/s is close in magnitude to the gravidynamic constant of 2.16.10*8 cm/s, which is included in the equation similar to the equation of the Lorentz force, which was calculated power gravimagnetic braking.

      1. Introduction

      "Does the gravitational field of the similarity with magnetic? Turn any electrical charge, and you get a magnetic field. Turn any mass, and, according to Einstein, you have to detect very weak effect, something similar to magnetism" is so popular NASA has justified the need to launch several satellites to detect effects of gravimagnetism. We are talking about the launch of the satellite gravity probe B (Gravity Probe B), in which gravimagnetic effect is expected to detect at the exact precession of gyroscopes mounted on the satellite [1]. In another experiment (frame-dragging), associated with the launch of two geodynamic satellites Lageos-1 and Lageos-2 (LAGEOS and LAGEOS II), it was shown [2] that the precession was only 20 % of the level predicted by the theory.

      Gravimagnetic effect can be detected not only by the precession of gyroscopes or "rotating frame", but also for deceleration or acceleration of the satellite depending on the direction of the force lines of the gravitational field and the direction of motion of gravitating bodies. Seems anomalies in the movement of the "Pioneers" in their acceleration or deceleration depending on the position in respect of gravitating bodies are also a consequence of gravimagnetic interaction [3].

      In this work the effect of gravimagnetism is considered on the example of anomalously high speed braking satellites of the moon and the laws of planetary and satellite distances, which, as it turns out, is also related to gravimagnetism through the rotation parameters central bodies.

      2. Gravimagnetic power

      Continuing the analogy with electrodynamics, braking force when interacting gravitating bodies can be expressed by the formula similar to the known electrodynamics equation of the Lorentz force:

      fgm = (v/C)2(GMm/r2)Sin α, (1)

      Where f is the force gravimagnetic interaction of bodies with masses M and m, remote distance r squared and moving relative to each other with velocity v in the direction at an angle α to the intensity vector gravimagnetic field, G is a gravitational constant and C is a constant with the dimension of velocity cm/sec. This will Illustrate scheme, see 1 a and b.

      Fig.1. Scheme of occurrence gravimagnetic forces: (a) a body with mass m, moving with velocity v in a gravitational field G, generates gravimagnetic field intensity H and the force f; (b) gravimagnetic force f (perpendicular to the plane of the drawing up) has a maximum value when α2 = 90° and sinα = 1, the reduction of the angle α leads to a decrease in f, if α = 0 the force f is also zero.

      Body m moves in a gravitational field G with velocity v at right angles to the power lines, Fig. 1a. The movement body m causes gravimagnetic field intensity H, the vector of which is directed normal to the vector of gravitational field strength G and the direction of body motion v. In this case, the moving body m will act normal to the direction of motion and the vector gravimagnetic tension braking force f. The magnitude of this force depends on the angle between the motion direction and the intensity vector gravimagnetic field H, see Fig.1 b. At α = 90° Sinα = 1, and the force f has a maximum value. When decreasing α below 90° decreases f and when α = 0 the braking gravimagnetic force disappears. The body moves in gravimagnetic field without resistance and energy consumption.

      To confirm advanced assumptions gravimagnetic braking bodies consider for example, at motion of satellites of the moon.

      3. Gravimagnetic braking satellites of the moon

      Starting with the first orbital flight of a satellite of the moon "Luna-10" [4, 5], which was launched on 3 April 1966, it became clear that the lunar satellites have abnormally high acceleration and the duration of their existence on the orbit is limited. Of all possible causes inhibition: perturbations due to the influence of the Sun and the Earth, the uneven distribution of mass, the presence of the moon, though very thin atmosphere, the impact of the solar wind – focused [6] non spherical shape of the moon. It was shown that perturbations caused by the non centric gravitational field of the Moon is 5-6 times larger than the perturbations due to the Earth's gravitation, and the latter exceeded the solar 180 times.

      The main reason for the occurrence of braking forces of the moon satellites may not be the uneven mass distribution, in particular the no spherical character of the Moon. Any algorithm for calculating the impact of uneven distribution of mass, the result depends on the mass of the satellite. The larger the mass, there is stronger interaction and the less the lifetime of satellites in orbit.

      However, the available data do not support this conclusion. For example, the satellite Kaguya" had a lot 2371 kg, and the duration of his stay in orbit amounted to 539 days, while the lunar Prospector", having mass 158 kg, ceased to exist after 182 days. As will be shown below, the deceleration time of the Moon satellites does not depend on their mass.

      The scheme gravimagnetic braking of the moon satellites is shown in Fig. 2. A satellite with mass m moves with velocity v, traversing radially spaced the force lines of the gravitational field G. The direction of the intensity vector occurring due to the motion of the satellite is perpendicular to the plane of the figure upwards. A satellite is braking by force f that causes the decrease of the orbital distances. By analogy with electrodynamics braking is accompanied by the gravitational radiation at a rate equal to the constant C in equation (1).

      Fig. 2. Scheme gravimagnetic braking the lunar satellite: a satellite with mass m moves with velocity v, traversing radially spaced force lines G of the Moon gravitational field (M); the direction of the intensity vector gravimagnetic field arising due to the motion of the satellite perpendicular to the plane of the drawing up; a satellite is retarding force f that causes the decrease of the orbital distance.

      Braking force satellite f in addition to equation 1 can be expressed by the equation of momentum:

      ft = m(v2 – v1), (2)

      where m is the satellite mass, t is the time of braking, v1 and v2 are the velocities before and after braking. Combining equations (1) and (2) obtain a convenient expression for calculating the

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