Amodel rocket is constructed with a motor that can provide a total impulse of 35.0 n·s. the mass of the rocket is 0.192 kg. what is the speed that this rocket achieves when it is launched from rest? neglect the effects of gravity and air resistance.

This is what i found “in a gas turbine engine, the combustor or combustion chamber is fed high pressure air by the compression system. early gas turbine engines used a single chamber known as a can type combustor. today three main configurations exist: can, annular and cannular (also referred to as can-annular tubo-annular).” i hope this you for what your looking for. can you plz mark me brainliest?