Posted by Malcom on Thursday, April 23, 2009 at 12:55am.
You want the space statiion to rotate at angular rate w such that
R w^2 = g, where R = 25 m.
Therefore w = sqrt(g/R).
Treat the space station as a wheel with all of its mass at distance R from the center. Its moment of inertia wil them be
I = M R^2
The "torque impulse" applied by the rockets in 1 hour must be enough to provide the required angular momentum of the space station, which is I w.
4 T R *(3600 s) = I w = M R^2 w
Solve for the thrust, T. The number 4 comes from the number of thrusters
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