Rocket Problem -- Solve using the Rocket Equation

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Homework Help Overview

The discussion revolves around a rocket problem involving the application of the rocket equation to determine the final velocity of a rocket after fuel consumption. Participants are exploring the implications of various parameters in the equation and questioning the validity of the initial problem setup.

Discussion Character

  • Mixed

Approaches and Questions Raised

  • Participants are attempting to apply the rocket equation and are questioning the inputs used in the calculations. There is a discussion about the mass flow rate and its impact on the rocket's acceleration and final velocity. Some participants are also reverse-engineering the problem to identify discrepancies in the provided answer.

Discussion Status

The discussion has highlighted various interpretations of the problem, with some participants suggesting that the original question may be flawed. There has been an acknowledgment of the need for clarity in the inputs to the rocket equation, and some guidance has been offered regarding the acceleration calculations.

Contextual Notes

There are concerns about missing information and the assumptions made in the problem setup, particularly regarding the mass of the fuel and the acceleration of the rocket during flight. The thread has also experienced moderation, indicating potential issues with the quality of responses.

mannerplay
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Homework Statement
Halliday Principles of Physics 10th edition
The mass of the rocket is 50 kg, the mass of the fuel is 450 kg
the rocket's maximum v rel=2 km/s
if R=10kg/s, what velocity does the rocket moves when it consumes all its fuel?
solve when the acceleration of the rocket is 20 m/s^2
Relevant Equations
Ma=-Rv (R is the ratio which a rocket's loss of its mass and v is the relative speed of the fuel to the rocket)
I tried the second rocket equation

vf = vi + v rel * ln(Mi/Mf)

but it gives out approximately 4900 m/s for the answer
but the answer is 4160 m/s
 
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What are ##v_i##, ##v_\text{rel}##, ##M_i## and ##M_f##?

You claim to have put them into the equation: ##v_f=v_i + v_\text{rel} \times ln(\frac{M_i}{M_f})## but I cannot tell what inputs you used to that equation.

If I reverse-engineer the supposedly correct answer, I come up with a different problem where the mass of the fuel is only 350 kg.

I have not been able to reverse-engineer your answer to see what you did. That is why it is important to show your work.
 
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mannerplay said:
if R=10kg/s, what velocity does the rocket moves when it consumes all its fuel?
solve when the acceleration of the rocket is 20 m/s^2

For starters if we are using the relevant equation as written ##R = -10 ~ \rm{\frac{kg}{s}}##
OR we leave ##R## positive and note that ##v_{e/R} = -2000 \rm{ \frac{m}{s} }##. Either way we note that the acceleration of the rocket is in the direction of motion for the rocket - not against.Next, I believe either the question is flawed OR they are two separate questions.

1) What velocity does the rocket moves when it consumes all its fuel?

2) What is its velocity when the acceleration of the rocket is 20 m/s^2? ( Flawed )

EDIT: Question 2 is flawed because the acceleration of the rocket is not less than ##40~ \rm{ \frac{m}{s^2} }## over the duration of powered flight.

$$ \left. \frac{dv}{dt} \right|_o = \frac{10~\rm{\frac{kg}{s}} 2000~\rm{ \frac{m}{s}} }{ 450~\rm{ kg } + 50~\rm{kg}} = 40~ \rm{ \frac{m}{s^2} } $$

$$ \left. \frac{dv}{dt} \right|_f = \frac{10~\rm{\frac{kg}{s}} 2000~\rm{ \frac{m}{s}} }{ 50~\rm{kg}} = 400~ \rm{ \frac{m}{s^2} } $$

Obviously that last one (the final acceleration at burnout) is a touch unrealistic!

Didn't realized this thread was dated...
 
Last edited:
Thread closed temporarily for Moderation...
 
Update -- this thread was probably doomed from the start because of the flawed OP question. A number of unhelpful replies have been deleted and the thread will remain closed now. Thanks.
 
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