Answer:
[tex]\omega=0.92rad/s[/tex]
Explanation:
The equation that relates rotational speed  with centripetal acceleration is [tex]a_{cp}=\omega^2r[/tex]. For our case we want to know how much has to be the rotational speed of the ring module of radius [tex]r=11.6m[/tex] in order  to achieve a centripetal acceleration equal to [tex]g=9.8m/s^2[/tex], which will be the acceleration felt by the astronauts.
We write then our equation as:
[tex]\omega=\sqrt{\frac{a_{cp}}{r}}[/tex]
Which for our values is:
[tex]\omega=\sqrt{\frac{a_{cp}}{r}}=\sqrt{\frac{9.8m/s^2}{11.6m}}=0.92rad/s[/tex]