kev said:
Your equation:
a_0=-\frac{m}{r^2}\frac{\sqrt{1-2m/r_0}}{1-2m/r}
does not work, because the proper acceleration of a free falling particle is zero. (Attach an accelerometer to a free falling particle and see what it reads.)
starthaus said:
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The math used for deriving the proper and coordinate acceleration in the radial field does not support your claim above. If you think otherwise try deriving the formula for the proper acceleration of a particle dropped from r=r_0 in a variable field as a function of the radial coordinate r. Show that your obtain a_0=0 for any r
Others have already correctly stated that the proper acceleration of a particle in freefall is zero by definition, but I accept your challenge for the more general case. This is not a formal derivation or proof. Just my best shot based on my physical understanding of the situation and my interpretation of the equations given by references like mathpages. (i.e. using selective "cut and paste" from the mathpages+hacks.)
For easy visualisation, consider the case of a small rocket descending into a gravitational well, with its thrust (Fo) directed in the opposite direction to the local gravitational acceleration (a'_g) so that the descent acceleration of the rocket at r, as measured by a stationary observer at r, is d^2r'/dt'^2 using his local clocks and rulers. (All primed variables indicate measurements made by a stationary local observer at r in the Schwarzschild coordinates). I can now say:
F_o = \left( \frac{d^2r'}{dt' ^2} - a'_g \right) m_o
where Fo is the proper force directed upwards and m_o is the rest mass of the rocket .
Dividing both sides by m_o gives the proper acceleration a_o of the rocket as:
a_o = \frac{d^2r'}{dt' ^2} - a'_g
where positive acceleration is defined here as upwards and negative acceleration means downwards.
A combination of http://www.mathpages.com/rr/s6-07/6-07.htm" gives the velocity dependent Schwarzschild coordinate gravitational acceleration a_g as:
a_g = - \frac{M}{r^2}(1-2M/r)\left(1-\frac{3(dr/dt)^2}{(1-2M/r)^2}\right)
Assuming the following relationships between the local vertical measurements (dr’, dt’, a’) made by a stationary observer at r and the coordinate measurements (dr, dt, a) made by a Schwarzschild observer at infinity using the gravitational boost factor \gamma_g = 1/\sqrt{(1-2M/r)}:
dr' = dr \; \gamma_g
dt' = dt \; \gamma_g^{-1}
dr'/dt' = dr/dt \; \gamma_g^{2}
a' = a \; \gamma_g^{3}
it is easy to obtain:
a'_g = - \frac{M}{r^2}\left(\frac{1-3(dr'/dt')^2}{\sqrt{1-2M/r}}\right)
where dr’/dt’ is the descent velocity of the rocket as it passes radial coordinate r as measured by a stationary observer located at r.
The more general proper acceleration can now be expressed in the form:
a_o = \frac{d^2r'}{dt' ^2} - a'_g = \frac{d^2r'}{dt' ^2} + \frac{M}{r^2}\left(\frac{1-3(dr'/dt')^2}{\sqrt{1-2M/r}}\right)
When the rocket is holding position at r by using its thrust to hover at r, dr’/dt’ = 0 and d^2r'/dt' ^2 =0 and its proper acceleration is:
a_o = \frac{d^2r'}{dt' ^2} - a'_g = 0 + \frac{M}{r^2}\left(\frac{1-3(dr'/dt')^2}{\sqrt{1-2M/r}}\right) = \frac{M}{r^2}\frac{1}{\sqrt{1-2M/r}}
which is what most people here expect.
In the specific case of freefall only, dr’/dt’ can be calculated using:
\frac{dr'}{dt'} = {\frac{\sqrt{2M (1/r-1/R)}}{\sqrt{1-2M/r}}
where R is a constant parameter of the trajectory path representing the height of the apogee and the following relationship is true:
\frac{d^2r'}{dt' ^2} = - \frac{M}{r^2}\left(\frac{1-3(dr'/dt')^2}{\sqrt{1-2M/r}}\right)
When the rocket turns off its engines and falls freely in a vacuum, the proper acceleration of the rocket is:
a_o = \frac{d^2{r}'}{d{t}' ^2} - a'_g = \frac{d^2{r}'}{d{t}' ^2} + \frac{M}{r^2}\left(\frac{1-3(dr'/dt')^2}{\sqrt{1-2M/r}}\right) = 0
for all R>2m and r>2m.