Answer:
[tex]a_b=\frac{1}{4}a_0[/tex]
Explanation:
Since the centripetal force F_C is, in this case, the gravitational force F_G exerted by the planet, we can say that:
[tex]F_G=F_C\\\\\frac{GMm}{r^{2} } =ma_c\\\\\frac{GM}{r^{2} }=a_c[/tex]
In the case of the satellite A we have:
[tex]\frac{GM}{d^{2} } =a_0[/tex]
And in the case of the satellite B:
[tex]\frac{GM}{(2d)^{2} } =a_b\\\\\frac{GM}{4d^{2} } =a_b\\\\\frac{GM}{d^{2} } =4a_b\\\\[/tex]
Finally, using these two expressions, we obtain :
[tex]4a_b=a_0\\\\a_b=\frac{1}{4} a_0[/tex]
In words, the centripetal acceleration a_b is equal to one fourth of a_0.