In the 1960's how did they figure out how fast the rocket to the moon would go as it lost fuel gained speed? Or can this be done dynamically with one equation without a computer or even a calculator? For simplicity ignore wind resistance and say you only had to figure out how to just get it only into orbit: Since you have the constant of the thrust of the engines is the same all the way to orbit, but speed is changing, acceleration is changing as you go up. One way to figure out would be to break the problem down into sections: X amount of thrust and Y amount of weight for 10 seconds =Z, then you do for 20 seconds then 30 etc. To get an accurate measurement you would keep doing this calculation using smaller and smaller time intervals 10 sec 11 sec …
But how would you figure this out dynamically without having to keep doing the equation over and over with your accuracy limited by the number of times you do the equations. iE 120 seconds to orbit with a 1 sec accuracy would require doing the equation 120 times. Is it possible to do one "elegant" equation that's valid for anytime? OR does this have to be done using computers? Does this make sense? Its hard to explain. Since your weight is going down constantly your variables are constantly changing making the one you used 1 second at lift off not work 119 seconds after because the rocket is lighter. Related question: Did the Apollo computer have to figure this out so it knew exactly when to fire/stop the rockets or was a mainframe on the ground doing this and sending telemetry because calculating this as too complex for onboard computers?