How can I display(code) the outputs they are asking. I am physics major

Question

rocket = cylinder( pos=vector(0,0,0), color=color.red, size=vector(0.5,0.1,0.1),
                   velocity = vector(0,0,0), mass=100, fuel_mass=10.0,
                   make_trail = True, axis=vector(0,1,0) )

initial_mass = rocket.mass + rocket.fuel_mass
initial_fuel_mass = rocket.fuel_mass

graph(fast=True)
r_pos = gcurve(color=color.red)

exhaust_velocity = vector(0,-100,0)
mdot = 1.0 # Rate of mass loss per time.
dt = 0.001
t = 0
scene.camera.follow(rocket)

while (rocket.fuel_mass > 0):
    rate(500)
    dm = mdot*dt # Amount of mass lost in time dt.
    rocket.velocity = rocket.velocity + dm/(rocket.mass+rocket.fuel_mass)*(-exhaust_velocity)
    rocket.pos = rocket.pos + rocket.velocity*dt
    rocket.fuel_mass = rocket.fuel_mass - dm
    rocket.opacity = rocket.fuel_mass/initial_fuel_mass
    t = t + dt
    r_pos.plot(pos=(t,rocket.pos.y))

print(rocket.velocity.y,mag(exhaust_velocity)*log(initial_mass/rocket.mass))  

#-----CALCULATING RANGE, TIME OF FLIGHT, MAXIMUM HEIGHT, LANDING VELOCITY FOR DIFFERENT VALUES OF INITIAL VELOCITY RELATIVE TO TERMINAL VELOCITY------#
low=alpha-0.5
intermediate=alpha
high=alpha+0.5

for vfactor in [low,intermediate,high]:
  velocity=vfactor*vt*vector(cos(theta), sin(theta), 0)
  #constants for drag force
  B1=m*mag(g)/vt
  B2=m*mag(g)/(vt**2)
  #drag forces
  Fdrag1=-B1*velocity
  Fdrag2=-B2*(mag(velocity)**2)*norm(velocity)
  print('For vfactor =', vfactor, '\n')
  
  print('For motion without drag forces :')
  projectile_cal(vector(0,0,0))
  print('\nFor motion with linear drag force, FD1 = -beta1*v :')
  projectile_cal(Fdrag1)
  print('\nFor motion with quadratic drag force, FD2 = -beta2*(v^2)*norm(v) :')
  projectile_cal(Fdrag2)
  print('-'*80, '\n')

I have the simulation, but i don’t know how to display results/outputs. I don’t know how to connect the dots, if you know what i mean. Thank You.

Use characteristics similar to the Falcon 9 rocket for the following: Total Mass: 433,100 kg First Stage Propellant Mass: 321,600 kg Thrust: 7,607 kN Exhaust Velocity: 2,766 m/s

A) Calculations: i. Calculate how long it take for the rocket to burn through its fuel. ii. Calculate the final velocity of the rocket after all the fuel expended. B) GlowScript Simulation: i. Use GlowScript to simulate the motion of the rocket. Your simulation should calculate the following for each time step: position, velocity, acceleration, rocket mass. ii. Plot the position, velocity, acceleration, rocket mass as functions of time.