Mind you a very high exhaust velocity is very important (it increases the specific impulse of the fuel), that is one reason LH2 + LOX is so attractive.
LOL!!!
The higher the velocity the higher the Pressure, retard.
Because it's Pressure that creates thrust, via Force=Pressure x Area.
And the Area part of F=pa on a rocket is measured at the nozzle exit...
Guess why?
That's right; because its Force is created by Pressure on the atmosphere!
And ZERO atmosphere = ZERO Pressure; guess what happens when you multiply something by ZERO, dummies?
As for using LH2 as fuel; HAHAHAHAHAHA!
LOX was bad enough, but LH2?
GTFO!
Never happened, ever, except maybe in small prototypes... Though I can't really see why they'd bother with even them, what with liquid-fuelled rocketry being a known technical dead-end since the late 1950s...
Total sci-fi nonsense anyhow; you Clowns are FUNNY!
No contradictions as long as you're using the right terminology a shameless Liar.
Fixed your bullshit for you.
Anyhoo, you can't have meaningful pressure inside the combustion chamber/nozzle without back-pressure.
And you can't have back-pressure in a vacuum.
In fact, you can't show me that you can have combustion in a vacuum, either...
And Boyle's law also states you can't even have a gas AT ALL in a vacuum!
Again; you REALLY need to start working on that new set of laws of physics, Clowns...
Cos the ones we've currently got simply will not let ypuu hazz shpayzeshippz!