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  A
				Mathematical Explanation of the Orbital Distance of
				Mercury
  by
				Miles Mathis
 
   
				
  
				 
				Abstract:
				I will show precisely why Mercury is orbiting at the distance it
				is, rather than at any other distance. 
				 
				I
				said in my Third Wave
				Series that I would have more to say about the mechanics of
				the Solar System, and this paper will be the first in a series
				explaining the Celestial Mechanics of near-space in a new and
				more rigorous manner.  In
				other papers I have shown that many “coincidences”
				are not coincidences but the outcome of simple interactions, and
				here I will continue to do that, with very simple math. 
				Historically,
				the orbital distance of Mercury from the Sun has been considered
				an accident, like all orbital distances. Currently, the standard
				model cannot tell us why the orbital distance of Mercury is what
				it is. Using my new Unified Field, I can. The standard model
				cannot explain the orbital distance using simple mathematics,
				since it does not have the correct fields.  The standard model
				explains the orbit using only two vectors, the centripetal
				acceleration caused by gravity and the orbital velocity of the
				planet.  But the gravity vector in the standard model has no
				mechanical life of its own.  The gravity vector is only an
				outcome of the orbital velocity. The gravity vector is not
				measured independently, nor is it theorized independently.  Both
				historically and mathematically, the gravity vector was arrived
				at by solving down from the orbital velocity, using the equation
				a = v2/r.*  The orbital velocity is the data (from the
				raw orbital period).  It is what is seen and measured.  The
				gravity vector only balances the orbital velocity.  It is an
				outcome, not a postulate.  This was true for Newton, it was true
				for Einstein, and it is still true for the standard model.  Up to
				now, there has been no real theory of gravity and no real
				mechanics underlying the vector. 
				 
				But
				I have shown in many
				other papers that the gravitational field is actually a
				compound field made up of two separate vectors. One of these
				vectors I continue to call gravity, since it is an apparent
				attraction. In the Unified Field, this vector points in. I call
				it solo
				gravity, since it is the gravitational field without the second
				field. The second field is the foundational
				E/M field or charge field. This is the field that underlies
				both electricity and magnetism, and mechanically it causes the
				charge between proton and electron.  I have shown that although
				the electrical field may appear to be either negative or positive
				in interactions, the foundational E/M field is always positive or
				repulsive.  It is caused by simple bombardment, via a particle I
				have dubbed the B-photon.
				This B-photon
				replaces the virtual photon or messenger photon of the standard
				model.  I also call it the charge photon in later papers.  All
				real photons in the spectrum can act as charge photons, and most
				do.  Although the charge field peaks or averages in the infrared,
				any photon that passes through the nucleus (during charge
				recycling) is part of the charge field.  
				 
				Since
				the foundational E/M field is always repulsive, it acts in vector
				opposition to the solo gravity field.  Both fields are active at
				all levels of size, cosmic and quantum. 
				 
				I
				have shown how these fields are both found in Newton’s
				gravitational equation. In the first instance, I have not added
				any terms to Newton’s equation: it still stands as it
				always has. I have simply broken it down into its constituent
				fields, showing how G
				works in the equation as a transform between the solo gravity
				field and the foundational E/M field. 
				 
				Once
				the two fields are separated, the solo gravity field turns out to
				be determined by radius alone. Gravity is an acceleration and
				nothing more. To be rigorous, it is the acceleration of a length
				or differential. This means it has nothing to do with density. 
				Density is a part of Newton’s equation, since it is a part
				of the mass variables, but it turns out that the density buried
				in the equation is actually a density of the foundational E/M
				field.  It is a density of B-photons. All you have to do
				is write each mass in Newton’s equation as density times
				volume, giving the density to the E/M field and the volume to the
				gravity field. G then acts as the transform between the two
				fields. I have shown that G is also the relative diameter of the
				B-photon. In other words, the B-photon is 6.67 x
				10-11 times smaller than the hydrogen atom. 
				 
				Those
				who have found my theory and math in these other papers to be a
				bit abstract may be interested to see the field applied to a
				standing problem of the solar system.  I will do that now.  I
				will show that the orbital distance of Mercury is the distance of
				balance for the three vectors involved. 
				 
				If,
				as I have claimed, the solo gravity field is determined by radius
				alone, we should be able to find an acceleration at the distance
				of Mercury quite easily, and it should not be the same as the
				current number.  In
				another paper I have shown that the solo gravity field of the
				Earth is not 9.81, but 9.82, and that the foundational E/M field
				of the Earth is -.009545.  If these figures are correct, I should
				be able to use these figures along with the known parameters of
				the Sun to find its
				separate fields.  If these two fields do balance at the distance
				of Mercury, I think I will have gone a long way to convincing
				skeptics, since only the correct mechanics could hope to solve
				the problem in this way. 
				 
				The
				Sun’s radius is 109 times that of the Earth.  If gravity is
				dependent upon radius alone, then the Sun’s gravitational
				acceleration at its surface must be 109 times that of the Earth,
				not 28 times as the standard model tells us.  If so, then its
				surface gravity must be 1070 m/s2, not 274 m/s2.
				 If that is true, then at the distance of Mercury, this
				acceleration would be: 
				(1070
				m/s2)(696,000/5.8 x 107)2 = .154
				m/s2 
				The
				standard model currently believes the acceleration at the
				distance of Mercury is: 
				Orbital
				velocity of Mercury = 48,000 m/s 
				a
				= v2/r 
				a
				= (48,000 m/s)2/(5.8 x 1010m) 
				a
				= .04 m/s2 
				The
				dirty little secret here is that the standard model believes the
				surface gravity of the Sun is 274 m/s2 simply because
				they did this math backwards. NASA has never measured the surface
				gravity directly, of course. That number 274 is arrived at by
				working backward from the orbital velocity of the planets.  It is
				not a measured number, it is a calculated number.  And it
				is calculated by assuming that gravity balances the
				orbital velocity directly.  The standard model has never proved
				that gravity does this, it simply calculates the number required
				to balance the orbital velocity and calls that number gravity. 
				There is no mechanics involved. 
				 
				But
				in my theory, all the numbers are grounded by field mechanics. 
				If gravity is dependent on radius alone, we have a logical field
				from the beginning.  Gravity is an acceleration in the equations,
				and now in my equations it is an acceleration in the field as
				well.  It is an acceleration and nothing else.  It does
				not include density, so it has no mystery to it anymore.  Where
				Newton and the standard model have much to explain, I have
				nothing to explain.  My solo gravity field has nothing to do with
				mass or density, so most of the historical questions immediately
				evaporate. 
				 
				Can
				my mechanics explain the balance better than the standard model? 
				You be the judge. I have shown that the gravitational strength at
				the distance of Mercury should be .154 m/s2 and that
				Mercury’s orbital velocity tends to give it an escaping
				force of .04 m/s2.  Therefore, the E/M field must make
				up the difference.  That is, I must find that 
				.154
				m/s2 + E = .04 m/s2 
				E
				= -.114 m/s2 
				I
				must show that, at the distance of Mercury, the Sun is repulsing
				at that strength.  We can do that in two ways.  One, use that
				number to show what the Sun must be repulsing on its surface: 
				ES
				(696,000/5.8 x 107)2 = -.114 m/s2 
				ES
				= -792 m/s2 
				Or,
				go to the surface directly, and figure from the surface numbers: 
				1070
				m/s2 + ES = 274 m/s2 
				ES
				= -796 m/s2 
				To
				balance the orbit of Mercury we must find that value for ES.
				 Is it possible that this value confirms my value for the Earth
				of -.009545 m/s2?
				 I found that value for the Earth simply by looking at the
				parameters of the Earth and Moon, as you can see by returning to
				that paper.  That
				paper was written several years ago, and when I wrote it I had no
				idea it would be useful when looking at Mercury or the Sun.  Many
				will have thought I pulled that number out of a hat, by some kind
				of magic (although the math is quite simple); but if I can use it
				to balance the orbit of Mercury, many people will be eating their
				own hats. 
				Watch
				this: 
				I
				showed that the foundational E/M field of the Earth has a
				strength at the surface of the Earth of -.009545 m/s2.
				 The Sun has a mass of 333,000 Earths.  It has a density ¼
				that of the Earth. 
				 
				(-.009545
				m/s2)(333,000)(¼) = -795 m/s2 
				No
				magic there, just transparent math and fully defined field
				mechanics. By these calculations, the Sun is “attracting”
				Mercury with a straight acceleration of .154 m/s2.  It
				is repulsing Mercury by bombarding it with B-photons at a
				rate of -.114 m/s2.  Mercury is fleeing the Sun at a
				rate of .04 m/s2. These three vectors balance at the
				orbital distance of 58 million kilometers.  That is the
				mechanical reason Mercury is at that distance and at no other
				distance. 
				 
				All
				this was made possible by mechanical postulates.  I did not start
				with orbital velocities and solve down from them, like Newton and
				the standard model.  I started with the theoretical postulate,
				based on logic, that gravity, taken alone, must be proportional
				to radius and radius only.  If gravity is an acceleration in our
				math, we should attempt to make it an acceleration in our
				mechanics and fields, unpolluted by other factors like density. 
				If Einstein was correct in his equivalence principle—and I
				believe that he was—then gravity should be expressed by
				acceleration alone.  If we follow Einstein’s lead and
				reverse the gravity vector, then the acceleration must apply to a
				length, not to a mass.  If we reverse the vector g, then
				it must be the acceleration of the radius. The equivalence
				principle is equivalent only if the vector applies to the same
				parameter in both directions, both before and after the reversal.
				 The acceleration and gravity vectors are equivalent and
				reversible only if they both apply to lengths.  We must have the
				acceleration of a length in both directions.  In other words,
				when we treat gravity as a pull down, we do not have to consider
				the mass of the object being pulled.  All objects,
				regardless of mass or density, are pulled down at a rate of 9.81
				on the surface of the Earth. Therefore, if we reverse the vector,
				we should not have to take the mass or density of the Earth into
				consideration.  If we reverse the vector, a la Einstein,
				the Earth is then expanding.  But the acceleration is given to
				the radius and the radius only.  Logically then, gravity should
				vary with radius. 
				 
				This
				postulate, applied to Earth and Moon, allowed me to generate
				numbers for both fields in my Unified Field. The only other
				postulate necessary was that the E/M field filled the gap, and
				did so by being always repulsive, in vector opposition to
				gravity. This postulate was not pulled from thin air, either. It
				was a logical requirement of the charge field. Up to now, the
				charge field has been mechanically undefined.  It has been
				mediated by virtual particles, which created a force and a field
				with no mass and no energy.  Impossible.  I simply gave this
				field the energy required to make it work mechanically, and that
				energy had to be inserted into the universe. It could not exist
				at the quantum level and fail to exist at the macro-level. I
				inserted it into Newton’s equation, and it happened to fit
				quite well. Since I had already changed the strength of solo
				gravity, there was plenty of room in Newton’s equation. The
				foundational E/M field fit the empty space like a hand in a
				glove.  In this way I was able to keep Newton’s compound
				field exactly like it was.  I made no correction to Newton, I
				simply re-expanded his equation, showing its constituent parts. 
				 
				 
				One
				final clarification. Some will see my equation above and ask why
				it cannot be applied to the Moon.  To find the number for the
				Sun, I multiplied the Earth’s E/M field by the mass
				differential and the density differential.  If we do that for the
				Moon, we get 
				 
				(-.009545
				m/s2)(1/81)(.6) = -.00007 m/s2 
				But
				I have shown in another paper that the Moon’s E/M field is
				actually greater than the Earth’s, with a number of -1.05
				m/s2.  How do I explain this?  I explain it because,
				as I have said before, you can’t just start plugging
				numbers into equations.  You have to look at how the field
				mechanics are working beneath the equations.  These differentials
				are relative numbers, and in one case we are looking at an object
				smaller than the Earth, the Moon; in the other case we are
				looking at an object larger, the Sun. And I have shown that the
				Unified Field unifies differently at different sizes. This is
				because we aren’t concerned directly with the macro-density
				of the macro-object, we are concerned directly with the density
				of the bombarding field of B-photons. In a smaller
				spherical object, this field is automatically compressed on the
				surface of the object, due to the surface area only. Our
				equations must therefore express this.  In other words, if the
				Sun and Moon had the same density, they still would not have the
				same E/M field density.  The E/M field density is not dependent
				upon object density, it is dependent on mass and surface area. 
				The entire mass emits the field, and it emits it into a certain
				space.  The Moon is emitting into a very small space compared to
				the Sun, you see. Therefore, all other things being the same, the
				Moon must have a denser field. 
				 
				Of
				course all other things are not the same, since the Sun has a
				mass 27 million times that of the Moon.  It has a huge amount of
				mass summing behind the surface, and this takes the strength of
				the Sun’s E/M field back above that of the Moon, by a large
				margin (757x).  It may seem strange that both the Sun and Moon
				have stronger E/M fields at their surfaces than the Earth, but if
				you do the math and follow the fields, it makes perfect sense. 
				 
				Let’s
				look at the surface area differential in both problems, to show
				this. To find the Sun’s E/M field from the Earth’s,
				you can multiply by the mass differential and the density
				differential, as I showed. But, although this is the most
				efficient method, it does not show the mechanics as clearly.
				Using the surface area differential, we would expand the
				transform for the Sun like this: 
				(-.009545
				m/s2)(SA)(D) x (M)/(SA) = -795 m/s2 
				The
				first term, SAD, gives us the density of the macro-field on the
				surface; and the second term, M/SA, gives us the strength of the
				B-photon field backing up or feeding that surface area.
				The two together give us the E/M field strength at the surface. 
				 
				But
				if we do the same thing with the Moon, we cannot use the same
				equation.  Instead we must use this equation: 
				(-.009545
				m/s2) (SA)M/D x (SA)/M = -1.05 m/s2 
				The
				second term is the inverse, as you see, since we must find the
				field feeding the surface. And the first term is also slightly
				different, since this term expresses the size difference. Objects
				larger than the Earth will be emitting into a larger space and
				objects smaller than the Earth will be emitting into a smaller
				space. Therefore, the transform must work differently in each
				direction. The Sun must have a less dense field on the surface,
				and the Moon must have a more dense field on the surface, and the
				equation must express this. We divide by the density instead of
				multiplying, as you see, and this expresses the move to smaller
				instead of larger.  But we need one final change, and that is to
				multiply by the mass differential once more. This is because if
				we divide by the density differential we lose the mass
				differential; so we need to reinsert it. Another way to look at
				it is that we really multiply by the volume differential when we
				go smaller. 
				 
				(-.009545
				m/s2) (SA)V x (SA)/M = -1.05 m/s2 
				That
				keeps the field mechanics in order. I know this last part is a
				bit dense, but if you study the mechanics—as I have
				described it above and in several other papers—you will see
				why transforming smaller and transforming larger, using the field
				differentials, must be done with different equations. Remind
				yourself occasionally that these variables do not stand for the
				actual densities or volumes or masses.  In these equations they
				stand for the relative numbers: one object’s mass relative
				to the other object’s mass, for instance. 
				 
				
  
				 
				*Some will be
				surprised to find me using the equation a = v2/r, when
				I have shown that it is false. I must use it in this paper,
				simply because I am using numbers derived from it, like the
				orbital velocity of Mercury. The number 48,000 isn’t really
				the orbital velocity of Mercury, it is 2πr/t for Mercury. 
				Although the term 2πr/t isn’t the orbital velocity, it
				is the term that works with a = v2/r, so if I am going
				to use one I must use the other. 
				 
				 
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