So; seems the 'nos' have it & the exhaust of a rocket produces no thrust after it has passed the rim of the nozzle.
In which case, let us now turn to the V2 rocket;
www.v2rocket.com has all the technical details we require.
Note that the combustion chamber & nozzle are fixed & immobile.
Then note the 4 carbon graphite
exhaust rudders placed
outside the rim of the nozzle.The purpose of these rudders is
THRUST VECTORING (definition of vectoring: 'directing to a desired point') in order to steer the rocket, by
directing the exhaust gases.
Even wikipedia agrees on this.
But, according to the model of all those who answered 'no', this is clearly impossible as you all agree that
the exhaust of a rocket produces no thrust after it has passed the rim of the nozzle.So; logically, as there would be no THRUST to VECTOR, either the steering system of the V2 did not & could not work as claimed, or you are wrong.Which one is it?