Answer:
a = 1.709g
Step-by-step explanation:
Given the absence of external forces being applied in the space station, it is possibly to use the Principle of Angular Momentum Conservation, which states that:

The required initial angular speed is obtained herein:




The initial moment of inertia is:



The final moment of inertia is:



Now, the final angular speed is obtained:



The apparent acceleration is:



This is approximately 1.709g.