Hi Folks;
I have a few questions regarding the maximum possible orbital velocity of a massive system around black holes.
But first, note that I am aware that the minimum distance for a non-accelerated circular stable orbit around a non-rotating black hole is r = 3GM/[C EXP 2] and the radius of a black hole photosphere is 3GM/{2[C EXP 2]}. For non-rotating black holes, the radius of the photosphere is 1.5 times that of the Event Horizon.
Since the velocity of light at the photosphere of the black hole is sufficient to permit the light to travel stable orbits around a black hole, would not a space craft with a suitably accelerated motion be able to maintain stable circular orbits with a radius as small as that of the photosphere for the case of a non-rotating black hole. I assume that the velocity of such a space craft is limited to the speed of light in vacuu because the velocity of a photon in vacuu is sufficient to hold it in a stable circular orbit around the black hole.
As for the second question, could not a space craft maintaining a stable accelerated orbit of the same radius as that of the photosphere actually be able to obtain a maximum orbital velocity arbitrarilly close to the speed of light in vacuu or C.
The third question I have is related to scenarios of accelerated space craft orbits within the photosphere of a black hole where the orbits are elliptical. For such accelerated orbits, could not a space craft undergoing such an accelerated orbit for which the semi-major axis would lie within the photosphere for a non-rotating black hole experience an average general relativistic time dilation that is limited only by a bounding value of infinity with respect to an observer that is located well outside the photosphere of the black hole.
Note that for all three of the above inquiries, I am either neglecting the effects of space craft orbital energy losses as a result of gravitational radiation, or am assuming that an external power source can download energy into the space craft propulsion system so as to compensate for orbital energy level losses due to any excessive gravitational radiation emissions from the space craft.
I am also assuming that the mass of the black hole is sufficient so that the orbiting space craft would not be shredded by tidal forces. One scenario might entail the use of ultra-massive black holes with a mass of 10 EXP 11 solar masses or greater, but which have as of yet, obviously remain un-observed.
Thanks;
Jim
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