What is the equation for the velocity of a rocket as a function of time?

In summary: Then take it from there.In summary, the conversation discusses a problem where a rocket with a mass of 2,000 kg and 3,000 kg of fuel is drifting in space and then fires its engine. The conversation goes through a series of equations and steps to find the velocity of the rocket as a function of time. In the end, it is determined that the velocity of the rocket can be represented by the equation V=Kt+Vi, with K being a constant. However, this equation may not accurately represent the actual acceleration of the rocket.
  • #1
Samuelriesterer
110
0
I am stuck on how my teacher got to the last equation in #4.

Problem Statement:

A 2,000 kg rocket carrying 3000 kg of fuel is drifting in space when it fires its engine. While operating, the rocket engine burns 20 kg of fuel per second and the exhaust gasses leave the rocket at an exhaust velocity of Ve =300 m/s relative to the rocket.

Relative equations:

p = mv

Work done:

1) At some moment while the engine is firing, the rocket has mass M and is moving at velocity v, as is all the fuel it contains. After a short time Δt, the rocket has burned an amount of fuel Δm which leaves the rocket at velocity ve relative to the rocket. Write expressions for the total momentum before Δm is burned and after Δm is exhausted.

pi = MVi
pf = (M - ∆M)(Vi + ∆V) + ∆M(Vi –Ve)

2) Set the two expressions in (1) equal and expand any products of sums and differences.

(M - ∆M)(Vi + ∆V) + ∆M(Vi –Ve) = MVi →
M Vi - Vi∆M + M∆V +∆M∆V + ∆M Vi - ∆MVe = M Vi →
- Vi∆M + M∆V +∆M∆V + ∆M Vi - ∆MVe = 0 →
M∆V +∆M∆V - ∆MVe = 0

3) Delete any terms which are a product of two factors of Δm, Δv in any combination (they will be much smaller than other terms as Δt shrinks to zero).

M∆V +∆M∆V - ∆MVe = 0 →
M∆V - ∆MVe = 0 →
M∆V = ∆MVe

4) Now take a limit as Δt shrinks to zero and integrate from t = 0 to t to find an expression for the velocity of the rocket as a function of time.

M∆V = ∆MVe →

(M∆V)/(M∆t) = (∆MVe)/(M∆t) →

∆V/∆Vt = (∆MVe)/(M∆t) →

∆V/∆Vt = (Ve/M) (∆M/∆t) - Not entirely sure how he came to this or to the next equation:

V = Kt + Vi

5) Integrate from Δm = 0 to 3000 kg (t= 0 to [3000 kg/20kg/s]). to find the change in the velocity of the rocket.
 
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  • #2
Samuelriesterer said:
∆V/∆Vt = (∆MVe)/(M∆t) →

∆V/∆Vt = (Ve/M) (∆M/∆t) - Not entirely sure how he came to this
It's a simple rearrangement of terms:
##\frac{\Delta M V_e}{M \Delta t} =
\frac{V_e \Delta M }{M \Delta t}= \frac{V_e}{M} \frac{\Delta M }{ \Delta t}##
But don't you mean
##\frac{\Delta V}{ \Delta t} = \frac{V_e}{M} \frac{\Delta M }{ \Delta t}##?
Samuelriesterer said:
or to the next equation:
V = Kt + Vi
Are you sure you've quoted that correctly? What is K here? That equation looks like uniform acceleration, which is not what will happen.
 
  • #3
Sorry, the K I believe is a constant
 
  • #4
Samuelriesterer said:
Sorry, the K I believe is a constant
Well, as I said, that'd be wrong.
You have ##
\frac{d V}{d t} = \frac{V_e}{M} \frac{d M }{d t}##
What do you get by integrating that?
 
  • #5
##tV + C = (tVe)/(M) + C## ?
 
  • #6
Samuelriesterer said:
##tV + C = (tVe)/(M) + C## ?
No. You have
##\int \frac{d V}{d t}dt = \int \frac{V_e}{M} \frac{d M }{d t}dt##
Simplify both sides.
 

1. What is rocket velocity?

Rocket velocity is the speed at which a rocket is traveling through space. It is typically measured in kilometers per second (km/s) or miles per hour (mph).

2. What does the "Kt" in the equation represent?

The "Kt" in the equation represents the specific impulse (Isp) of the rocket. This is a measure of the efficiency of a rocket's engine and is typically given in seconds.

3. What does the "Vi" in the equation represent?

The "Vi" in the equation represents the initial velocity of the rocket. This is the velocity at the start of the rocket's flight, before any additional acceleration from the engines.

4. How is rocket velocity calculated?

Rocket velocity is calculated using the equation V = Kt * ln(Mo/Mf) + Vi, where V is the final velocity, Kt is the specific impulse, Mo is the initial mass of the rocket, Mf is the final mass of the rocket, and Vi is the initial velocity. The natural logarithm (ln) is used to account for the changing mass of the rocket as fuel is burned.

5. How does rocket velocity affect space travel?

Rocket velocity is crucial for space travel as it determines how far and how fast a rocket can travel. The higher the velocity, the farther and faster the rocket can go. It also affects the amount of fuel needed for a journey, as a higher velocity requires more fuel to achieve and maintain. Therefore, increasing rocket velocity is a major goal in space exploration to reach farther and more distant destinations.

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