Was Re: ZetaTalk and Spaceguard UK (D8) thread

Since no one else has taken a stab at computing the Repulsion Force R
factor, I'll do it.  A factor that would prevent the Moon from orbiting
the Earth at the level the satellites orbit, as it would only need to
hover.  A factor that would explain why the planets return to their
orbits after having been perturbed in closer to the sun, and be
sufficient to return them to their orbits.

    Where the repulsion force comes to equal the force of gravity
    by the time the objects in play would make contact, it builds
    at a rate that differs from gravity. ... The repulsion force is
    infinitesimally smaller than the force of gravity, but has a
    sharper curve so that it equals the force of gravity at the point
    of contact.
        ZetaTalk™, Repulsion Force

If
    Inverse Square      F = G*M1*M2/r^2
    Centrifugal Force   F = G*M2* v^2
    Velocity            v = sqrt(G*M1 / r)
    Orbit Constant     80 = M1*p^2 / r^3

Presume
    Inverse Square      F = (G*M1*M2/r^2) - R
    Centrifugal Force   F = (G*M2 - R/M1)* v^2)
    Velocity            v = sqrt(G*M1 / r) - sqrt(G*R /r)
    Orbit Constant     80 = M1*p^2 / r^3 - (R*p^2/r^3 - 80)

So where                r = 1 or the point of contact, then
    Inverse Square      F = 0 at the point of contact
    Centrifugal Force   F = 0 and an object need not orbit
    Velocity            v = 0  and an object can hover at ground level
    Orbit Constant      p = 0  and an object can hover at ground level

INVERSE SQUARE
                        F = (G*M1*M2/r^2) - R
                   so   R = (G*M1*M2/r^2) - F

        if F = 0 and
           r = 1 then

                        R = G*M1*M2

CENTRIFUGAL FORCE
                        F = (G*M2 - R/M1)* v^2)
                 so     R = (G*M2 - F/v^2) * M1

        if F = 0 and
           v = 0 then

                        R = G*M2*M1

VELOCITY
                        v = sqrt(G*M1 / r) - sqrt(G*R /r)
                  so    sqrt(G*R /r) = sqrt(G*M1 / r) - v

          if v = 0 and
             r = 1 then

                        R = M1

ORBIT CONSTANT
                        80 = M1*p^2 / r^3 - (R*p^2/r^3 - 80)
                  so    R*p^2/r^3 = M1*p^2 / r^3

          if r = 1 and
             p = 0 then

                        R = M1

So what is the R factor?