#Anyone know how I can use [v(t)]^2 for this rocket equation? I get stuck on
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basically I need to make a model that solves this:
when v(t) is not squared the answer is:
I need to be able to essentially plug in the initial mass of a rocket and the final mass of a rocket (no fuel) and some air resistance data and gravity, the flow rate of fuel, and the final (maximum delta V) should be the answer.
variable mass system right?