Originally posted by Roy
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I have found another problem with satellite orbits.
If you take the equations for orbital velocity around the barycentre in an n-body problem
(i) pv=nrt
(ii) v=ir
which show the relationships between orbital velocity and (i) the orbital radius and time, and (ii) the complex component of the elliptical radius, then
v=ir=nrt/p
so cancelling r
i=nt/p
or
t=pi/n
So for a 3-body interaction such as the sun-earth-moon complex, the orbital time t=pi/3=3.141/3=1.141
but the orbital time of Earth/moon around the earth/moon/sun barycenter is 1 year, not 1.141 years, so G and NM is invalidated.
If you take the equations for orbital velocity around the barycentre in an n-body problem
(i) pv=nrt
(ii) v=ir
which show the relationships between orbital velocity and (i) the orbital radius and time, and (ii) the complex component of the elliptical radius, then
v=ir=nrt/p
so cancelling r
i=nt/p
or
t=pi/n
So for a 3-body interaction such as the sun-earth-moon complex, the orbital time t=pi/3=3.141/3=1.141
but the orbital time of Earth/moon around the earth/moon/sun barycenter is 1 year, not 1.141 years, so G and NM is invalidated.
JM
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