Having tried to launch from Eve with a lander than can easily reach orbit from kerbin only to see it apogee at 20km was a bit disappointing. So this time I would like to actually calculate how much fuel I need to reach orbit with out getting at that number with trail and error. If I know the dry mass of my lander, twr, engine thrust and specific impulse, surface gravity and atmospheric drag. What formula would I use to calculate how much fuel I need to lift the craft to 120km orbit? Thank you