I do not understand your {\rm m} symbol.
Compute the required angular rotation rate w, in radians per second. Then convert that w rate to rpm. I assume you know how to d that.
The rate is given by
R w^2 = g
w = sqrt(r/R)
If a cylindrical space station 300 {\rm m} in diameter is to spin about its central axis, at how many revolutions per minute ({\rm rpm}) must it turn so that the outermost points have an acceleration equal to g?
2 answers
0.08