Answer:
The acceleration is

The velocity after 20 second is

Step-by-step explanation:
From the question we are told that
The mass of the rocket is

The rate of fuel consumption is

The speed of speed at which gas is ejected at atmospheric pressure is

Generally the thrust force (the force propelling the rocket) is mathematically represented as

=>

=>

Generally the net force acting on the rocket is mathematically represented as

=>
=>
=>

Generally the rocket speed is mathematically represented as
![v = v_i - gt + v_g * ln[(m)/(m_r) ]](https://img.qammunity.org/2021/formulas/physics/college/89d0d5uv9kskbrd100a2qip7iia9zhj80c.png)
Here
is the initial velocity of the rocket which is 0 given that it started from rest
of the rocket after fuel has been consumed for time t = 20
second, this mathematically represented as

=>

=>

So
![v = 800 - 9.8 * 20 + 3500 * ln[(800)/(700) ]](https://img.qammunity.org/2021/formulas/physics/college/i75so1r90r0jshtk268u6pgibt8mb9vhhb.png)
=>
