To calculate a delta-v for any space fiction getting out of a JGO you need to know your mass before/after activating your rocket engine and also the velocity of your exhaust. This according to comrade Tsiolkowsky. I think he is right and Gagarin faked it.
Incorrect!
You only need the mass before/after the burn (from the mass ratio) to find the fuel burn from the required delta-V.
Try again!
But since I never asked for a LEO of 100 km,
make it more practical and calculate the two delta-Vs needed to transfer from a circular LEO at 200 km to a circular GEO.
If you can't understand that and come up with an answer, you are a total fraud.
Well, the original question remains how to go from Low Earth Orbit, LEO, to Low Lunar Orbit, LLO. The answer is, of course, that it cannot be done at all.
If you manage to get off the ground and into LEO, you don't have the fuel to get out of LEO and later brake to get into LLO, if you reach the target. You are bound to crash or just disappear into the Milky Way.
Juri Gagarin just tried to get into and out of LEO 1961 and he was a total fraud. John Glenn copied it 1962 and he too was a total fraud. You sound like a twerp believing in Father Christmas and the Tooth Fairy.
Ok prove it. Show your evidence here, where you made the claim. There is no evidence on your pathetic website, there is only you whining like a little bitch that you can't understand it so it must be false.
Of course you will, as always, fail to back up your stupidity. This is because you are a liar, fraud, failure and idiot of epic proportions.
You could always prove me wrong and post your evidence here, but we both know that isn't going to happen for the reasons listed above.
So, you tiny brained stinking pile of shit, put up or shut up. I can keep this up as long as you can.
Prove me wrong or admit defeat.