Answer:
The required angular velocity (ω) will be
.
Step-by-step explanation:
Due to the rotation of the space station the astronauts experience a centripetal acceleration towards the centre of the space station. If '
', 'ω' and 'R' represent the centripetal acceleration, angular velocity of the space station and the radius of the space station respectively, then
![a_(c) = \omega^(2).R](https://img.qammunity.org/2021/formulas/physics/college/l7o86i1o23y13w7q65xu1uols7kgnx2a24.png)
As according to the problem the space station has to rotate in such an angular velocity that it produces the same "artificial gravity" as Earth's surface, we can write
![a_(c) = g = 9.8 ms^(-2)](https://img.qammunity.org/2021/formulas/physics/college/r4njjk5f7k7ej26lo10h0wkqz1zms5g1lg.png)
Also given
![R = (diameter~of~the~space~station)/(2) = (200 m)/(2) = 100 m](https://img.qammunity.org/2021/formulas/physics/college/ekidqh5udtra2lra8nsjh0axx75bbd9znh.png)
Therefore we can write,
![&& a_(c) = g = \omega^(2).R\\&or,& \omega = \sqrt{(g)/(R)} = \sqrt{(9.8 ms^(-1))/(100 m)} = 0.313~rads^(-1)](https://img.qammunity.org/2021/formulas/physics/college/2c6zffjrska4s2mmedoqg8mdobp5ca8eqf.png)