- #1

- 102

- 7

## Homework Statement

I'm having trouble deriving the equation for the velocity of a rocket in constant G given that it has constant exhaust velocity

## Homework Equations

I know that a=dv/dt=U/M(dM/dt)-g

## The Attempt at a Solution

so from here dv=U/M dM-gdt

v=U ∫1/M dM - g ∫dt v from 0 to v, M from Minitial to Mfinal, and t from 0 to t

which leads to v=-ln[Minitial/Mfinal]-gt

HOWEVER, everywhere I look, the answer is positive ln[Minitial/Mfinal] -gt and I can't seem to get why this is so