Thrust Question

1. The problem statement, all variables and given/known data
What thrust does a 200g model rocket need in order to have a vertical acceleration of 10.0m/s^2?
A) on earth?
B) on the moon, where g=1.62m/s^2

2. Relevant equations

3. The attempt at a solution
I am not sure of an equation to use for this problem

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