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... А Б В Г Д Е Ж З И К Л М Н О П Р С Т У Ф Х Ц Ч Ш Щ Э Ю Я

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Введите фамилию автора:

I must do my duty

I must do my duty



I.G. Goriachko, St. Petersburg, in February, 23.

Forms of neutral and changed body’s trajectories in Nature are very

differently and depended on a pressure (p) and temperature (T) of

surroundings. With reference to microcosm, the neutral bodies (photons,

roentgen-rays, gamma-rays, free neutrons, and etc.) for lack of influence

to them coulomb’s forces always moving merely by the parabolical

trajectories. The changed orbital bodies (electrons, protons, [pic]-

particles, and etc., being on the steady atom’s and nucleus’s orbits)

always moving merely by elliptical orbits. These changed particles by their

crossing from the one to the next steady elliptical orbit (and a free

changed ones) always moving merely by hyperbolical trajectories. As a

result of these crossings eccentricities of trajectories suddenly changed

from the range[pic]to the [pic][pic] (and back). This signified that

eccentricity (e) of the orbit is appeared as the quantum parameter depended

on (p, T). Into the atom and into its nucleus acted only exactly balanced

coulomb’s and gravity forces of differently ([pic]) orientations.

Therefore, so-called «nuclei ‘s forces» are not existing. The circle or the

straight-line motions in Nature are impossible in order to a really

curvature in space and time. But as natural indicator of this curvature may

be namely the form of body’s trajectory.

3.The real body’s trajectories in Nature

The explanation 2. It was shown in the exp. 1 for the orbital body: W < 0,

[pic][pic]for the non-orbital body: W>0, [pic]

Write down the conical equation (for the circle, ellipse, parabola,

hyperbola) in the non-dimensional forms

- for the ellipse

[pic] , where 0 <[pic], (2)

- for the hyperbola [pic] , where 1[pic]. (3)

By means of (2), (3),(A) we obtain

[pic] [pic], where [pic], (a)

[pic][pic] [pic], where [pic] (b)

For the straight-line: [pic] Therefore,[pic] (c). For the circle: [pic] .


For the parabola:[pic] Therefore,[pic](e). But for the elliptical and

hyperbolical trajectories parameters[pic]are periodical ones.

4.Some useful formulas

Cephler’s the Third law has the next modern form (where f – the gravity

constant, M – mass of the Sun, [pic] - the orbit ‘s semi-axis, [pic] –

period) [pic] But as w=[pic][pic] (where m – the planet’s mass) we obtain

from (1) [pic][pic] From these equations we obtain the correlation (A),

where [pic]. Also from the (1) we obtain: a)[pic] For the circle ([pic])

motion [pic] - the first cosmic velocity. For the parabolic ([pic]) motion

[pic] - the second (or so-called - the «parabolic») cosmic velocity, and

etc. b) [pic] (where M – the planet’s mass, r–the planet’s radius, [pic]the

basis vector). Therefore, the body’s weight ([pic]) on the planet depended

on the form its orbit. For the circle ([pic]) motion, we obtain: [pic] -

the acceleration of gravity. From the (B’) for the photon ([pic][pic]) , we

obtain : [pic]- the full photon’s energy. And etc. You will be certained

soon about the parameter [pic][pic] fundamental significance in

thermomechanics of macro- and microcosm.

Thank you. To the next report in March, 08. G.I.G.

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