Investigating a Rocket Launch Speed Anomaly

In summary, the conversation discusses the proper time between two events in Earth's frame of reference and how it is perceived in the frame of a rocket leaving Earth at a different velocity. The speed of the second rocket catching up with the first one is calculated and compared to the predicted result, with a clarification made about the distance and time used in the calculation.
  • #1
quasar987
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Is there something wrong with this reasoning:

First the question:

"A rocket A leave Earth at a speed v at a time where the clocks onboard and those on Earth read 0. After a time T (for the Earth's clock), a second rocket is lauched with a speed u > v. The second rocket catches up with the first one at a time t such that (t - T)u = tv, or equivalently, t = uT/(u-v)."

a) For the clocks on A, when does B leave earth?

MY ANSWER: The time between the events "A leaves" and "B leaves" is proper on earth. It is T on earth; therfor it is given on A by

[tex]t_A_1= T\gamma _{AT} = \frac{T}{\sqrt{1-(v/c)^2}}[/tex]

b) For the clocks on A, when does B catches up with A?

MY ANSWER: By Lorentz,

[tex]t_A_2 = \frac{1}{\sqrt{1-(v/c)^2}}(t-v(vt)/c^2) = t\sqrt{1-(v/c)^2}[/tex]

d) Deduce the speed of B as seen in frame A. Does the result agree with the law of addition of speed?

MY ANSWER: Speed of B = distance traveled in catching up with A / time took to do so

[tex]\Rightarrow v_{B \ in \ A} = \frac{vt_A_2}{t_A_2 - t_A_1}=\frac{vt\sqrt{1-(v/c)^2}}{t\sqrt{1-(v/c)^2} - T/\sqrt{1-(v/c)^2}} = \frac{vt}{t - T/(1-(v/c)^2)}[/tex]
[tex]=\frac{uv}{(u-v)(\frac{u}{u-v}-\frac{1}{1-(v/c)^2})}[/tex]

But according to Mapple (and to me), this is not equal to the predicted

[tex]v_{B \ in \ A} = \frac{u-v}{1-uv/c^2}[/tex]
 
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  • #2
quasar987 said:
MY ANSWER: Speed of B = distance traveled in catching up with A / time took to do so

[tex]\Rightarrow v_{B \ in \ A} = \frac{vt_A_2}{t_A_2 - t_A_1}=\frac{vt\sqrt{1-(v/c)^2}}{t\sqrt{1-(v/c)^2} - T/\sqrt{1-(v/c)^2}} = \frac{vt}{t - T/(1-(v/c)^2)}[/tex]

It should be:[tex]\Rightarrow v_{B \ in \ A} = \frac{vt_A_1}{t_A_2 - t_A_1}[/tex]

If you look at it from the frame of the rocket that left first... The other rocket leaves at t1. By that time the Earth has traveled vt1. So the distance between the two rockets is vt1.
 
  • #3
learningphysics said:
It should be:[tex]\Rightarrow v_{B \ in \ A} = \frac{vt_A_1}{t_A_2 - t_A_1}[/tex]

If you look at it from the frame of the rocket that left first... The other rocket leaves at t1. By that time the Earth has traveled vt1. So the distance between the two rockets is vt1.

Well yea...

But the time at the denominator is the time taken by the second rocket to catch up with the first. So the distance at the numerator should be the distance the second rocket traveled in catching up with the first one. And that distance is not vt1, because the first rocket continued to move during the time rocket 2 was catching up with it.

However vt2 gives the distance traveled by rocket 1 from the moment of its lauching to the moment it is catched up by rocket 2. So this has to be the distance rocket 2 has traveled to catch up with it.

Makes sense?
 
  • #4
quasar987 said:
Well yea...

But the time at the denominator is the time taken by the second rocket to catch up with the first. So the distance at the numerator should be the distance the second rocket traveled in catching up with the first one. And that distance is not vt1, because the first rocket continued to move during the time rocket 2 was catching up with it.

However vt2 gives the distance traveled by rocket 1 from the moment of its lauching to the moment it is catched up by rocket 2. So this has to be the distance rocket 2 has traveled to catch up with it.

Makes sense?

Not really.

Remember we are looking at this from rocket 1's frame of reference. So rocket 1 is at rest.

t2 and t1 are the times in the frame of rocket 1 right?

Remember that rocket 1 is at rest in rocket 1's frame of reference.

Look at this in rocket 1's frame of reference:
Rocket 2 is at a distance d from rocket 1, at time t1. Then Rocket 2 moves towards Rocket 1 till it reaches rocket 1. Rocket 2 reaches rocket 1 at time t2 in rocket 1's frame of reference.

What is the distance d? Isn't this just the distance between the Earth and rocket 1 at time t1?
 
  • #5
That makes a hell of a lot of sense now. You are a genius m8. :biggrin:
 
  • #6
quasar987 said:
That makes a hell of a lot of sense now. You are a genius m8. :biggrin:

Thanks. :smile: Glad to help!
 

Related to Investigating a Rocket Launch Speed Anomaly

Q: What is a rocket launch speed anomaly?

A rocket launch speed anomaly refers to a discrepancy or unexpected variation in the velocity of a rocket during its launch. This can occur due to a variety of factors, such as technical malfunctions, external influences, or errors in calculations.

Q: Why is it important to investigate a rocket launch speed anomaly?

Investigating a rocket launch speed anomaly is important for several reasons. Firstly, it can help identify any underlying issues or malfunctions that may have caused the anomaly, which can inform future rocket designs and launches. Additionally, understanding the cause of the anomaly can prevent potential accidents or failures in future launches.

Q: What are some possible reasons for a rocket launch speed anomaly?

There are several potential reasons for a rocket launch speed anomaly. These can include technical malfunctions, such as engine failures or fuel system issues, external factors like weather conditions or air resistance, or errors in calculations or programming.

Q: How do scientists investigate a rocket launch speed anomaly?

Scientists typically use a combination of data analysis, simulations, and physical testing to investigate a rocket launch speed anomaly. This may involve analyzing data from the rocket's launch and flight, conducting simulations to recreate the conditions and identify potential causes, and performing physical tests on components of the rocket to identify any malfunctions or failures.

Q: What are the potential outcomes of an investigation into a rocket launch speed anomaly?

The potential outcomes of an investigation into a rocket launch speed anomaly can vary depending on the cause of the anomaly. If the cause is identified and resolved, it can inform future rocket designs and launches to prevent similar issues from occurring. In cases where the cause cannot be determined, the investigation can still provide valuable data and insights for future launches.

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