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Some useful equations:

The specific impulse of a rocket propellant is defined as Isp = Fth / (Rg) , where Fth is the thrust of propellant, g is the magnitude of free fall accelaration at the surface of earth, and R is the rate at which the propellant is burned.

I have not shown any work because im lost as to how to start the problem. If more of an attempt is needed let me know and i'll post what I've done so far. Thankyou.