posted on Jul, 20 2017 @ 08:07 PM
I stated in a previous post in this thread that a rocket engine produces thrust mainly because of the pressure difference between the to sides of the
combustion chamber. One side high pressure and the other where the opening is low pressure with thrust being in the direction of the high pressure
In this post I am making a clarification. The low pressure side has to be at 0 or negative pressure for the thrust to occur.
For those attempting to design an inertial propulsion engine must take this concept into consideration.
edit on 20-7-2017 by eManym because:
(no reason given)