A rocket of mass burns of fuel per second. If the velocity of exhaust gas is , then it lifts with an acceleration of
Step 1. Given Data,
Let is the force on the rocket.
Velocity
Mass
Burned fuel per second
Step 2. We have to calculate the acceleration which lifts the rocket,
We know that,
Thrust force,
Now,
Then, the acceleration which lifts the rocket is .
Hence, the correct option is .