🚀 go-pugleaf

[GPSbob.wpd];             GPS & c^2 / f_b
The relative difference in the rate of a clock in a circular orbit of
EARth compared to a clock 'in' a Very Low Orbit (VLO) 'at' EQUiVALENT
radius as EARth (NOT "on" EARth's surface ..as some scientists say):
The GPS ATOMiC clock PREset Factor is 4.46 x 10^-10
            = (Very Low Orbit period tb) / (t1 - tb)
           = GPS orbital AMBiENT density / SURFACE AMBiENT density d3
      = (GPS AMBiENT particle COUNT/m^3) / Loschmidt's Constant ..no
            = (1.20 x 10^16 molpart/m^3) / (2.69 x 10^25 molpart/m^3)
                          = (v1^2 - vb^2) / 2*c^2
                          = (rA*gA - r3*g3) / 2*c^2
   = G*M1*[{1/(n1 - 1)*rA} - {1/(n3 - 1)*r3}] / c^2
                                       (fA - fb) / fb
= [{G*M1 / {(n1 - 1)*rA}} - {G*M1 / {(n3 - 1)*r3}}] / c^2.

1. CAViTY n=0 only & always in GR & Newton Tivity (BOTH ..no AMBiENT).
2. The GUESS Kinematic Viscosity & Diffusion factor = c^2 / fb
               = G*M1*[{1/(n1 - 1)*rA} - {1/(n3 - 1)*r3}] / (fA - fb).
3. v1^2 = G*M1 / (n1 - 1)*rA = rA*gA.
4. Vb^2 = G*M1 / (n3 - 1)*r3 = r3*g3 ..Note delta ALTiTUDE, (rA - r3).
5. The CAViTY n of n1 & n3 of mass m1 includes any m1 LATTiCE VACANCY.

M1 = Mass of EARth (here).
G = Gravitational Constant.
r3 = radius of EARth or rocket VLO.
rA = radius of orbiting clock's orbit.
v1 = 2*pi*rA/t1 = orbital speed of orbiting clock.
vb = 2*pi*r3/t3 = speed of the EARth clock (ECi frame).
v1^2 = rA*g = (vescape)^2 / 2*(n - 1) = G*M1 / (n - 1)*rA
[ m1*c/h=nL/wl=fL/c=pL/h=nA/2*pi*rA=eV/h*fA*rA=pA/h*rA ].
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