a rocket is ejecting 50g of gases per sec at speed of 500m/sec the acceleration force on rocket will be
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As we know force is product of mass and acceleration of an object.
F=ma
In above said case we can alter the equation slightly for given data, ie., F= mass flow rate x velocity.
F= Mv
M=Mass flow rate ( kg/sec), v=velocity (m/sec)
Let's do some calculations
F = (50×0.001)×(500)=25N
So the Thrust force of the rocket is 25N.
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