Rocket Motion in interstellar space

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Discussion Overview

The discussion revolves around the motion of a rocket in interstellar space, specifically focusing on the effects of gas ejection from a propulsion system on the astronaut's movement. Participants explore different methods to calculate distance traveled under varying mass conditions, addressing both theoretical and practical implications of their approaches.

Discussion Character

  • Exploratory
  • Technical explanation
  • Mathematical reasoning
  • Debate/contested

Main Points Raised

  • One participant suggests that if thrust is constant, the acceleration must increase as mass decreases, leading to a non-constant acceleration scenario.
  • Another participant questions how acceleration was determined using a method that assumes constant acceleration, which seems contradictory given the changing mass.
  • Several participants note that both methods (one assuming constant acceleration and the other using a logarithmic approach) yield the same final distance, which raises questions about the validity of the assumptions made.
  • There is a discussion about the necessity of using an average mass for calculations to reconcile the differing methods, as using initial mass alone may lead to discrepancies.
  • A participant highlights the presence of a logarithm in one method and seeks clarification on its derivation, linking it to the solution of a differential equation.

Areas of Agreement / Disagreement

Participants do not reach a consensus on the validity of the methods used. There is ongoing debate regarding the assumptions made about acceleration and mass, with multiple competing views on how to approach the problem.

Contextual Notes

Limitations include the dependence on assumptions about mass and acceleration, as well as the unresolved nature of the calculations presented. The discussion reflects uncertainty in the application of different mathematical approaches to the same physical scenario.

Who May Find This Useful

This discussion may be of interest to those studying rocket propulsion, dynamics in variable mass systems, or mathematical modeling in physics.

NATURE.M
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So suppose an astronaut in interstellar space has gas ejecting from her propulsion system.
So the gas would cause her to move forward by some distance, d. Then, the F_{thrust} acting on her must be constant (assuming the amount of gas ejected per unit time is constant, and the speed it is released at is constant). Then, since the mass of the system (astronaut+equipment) is decreasing the acceleration of the system must be increasing to enable the F_{thrust} to remain constant. Please correct me if my reasoning is wrong.

(1) So naturally it wouldn't be valid to calculate the distance she travels by finding the acceleration from Newtons second law, and using that along with a kinematical equation to solve for the distance d (since the acceleration isn't constant).
(2) So instead I would use v = v_{g}ln \frac{m_{i}}{m_{f}}, where v_{g} is the speed of the gas being ejected.
Then integrate for the position , x(t) = \int_o^t {v_{g}ln \frac{m_{i}}{m_{f}}}dt,
where m_{f}=m_{i} - \frac{dm}{dt}t, where \frac{dm}{dt} is the rate at which gas is ejected.

But then for a question I had to do, both methods (1 and 2) produced the same final answer which I found to be very odd. Any possible explanations?
 
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How did you figure an acceleration in order to solve the problem by the suspicious method 1?
 
dauto said:
How did you figure an acceleration in order to solve the problem by the suspicious method 1?

From F_{thrust}=\frac{dp}{dt} = \frac{d(mv_{g})}{dt} = v_{g}\frac{dm}{dt}
Then, a=\frac{F_{thrust}}{m_{i}}
And then x(t) = \frac{1}{2}at^{2}

Now this assumes the acceleration is constant, yet produces the same answer.
 
Last edited:
NATURE.M said:
From F_{thrust}=\frac{dp}{dt} = \frac{d(mv_{g})}{dt} = v_{g}\frac{dm}{dt} = ma
Then, a=\frac{F_{thrust}}{m_{i}}
And then x(t) = \frac{1}{2}at^{2}

If you used the initial mass than the two methods should give different results. You would have to use some kind of average mass in order for both methods to give the same solution. Why don't you post your calculations for the second method so that we may figure what's up?
 
Paying closer attention to your equations I noticed what seems to be a logarithm. Where did that come from?
 
dauto said:
If you used the initial mass than the two methods should give different results. You would have to use some kind of average mass in order for both methods to give the same solution. Why don't you post your calculations for the second method so that we may figure what's up?

Well let m_{i}=115 kg ,\frac{dm}{dt} = 0.007 kg/s,, v_{g}=800 m/s, t= 6 s .
Then, by method 1 F=5.6 N \Rightarrow a=0.0487 m/s^{2}\Rightarrow x= 0.877 m
, which is the same answer obtained by method 2.
 
dauto said:
Paying closer attention to your equations I noticed what seems to be a logarithm. Where did that come from?

By solving the differential equation \frac{dv}{dm}= -\frac{v_{g}}{m}.
 

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