Longitude contraction / time dilatation

AI Thread Summary
The discussion revolves around calculating the time taken for an observer in a spacecraft to reach Titan, as seen from both the Earth and the spacecraft. The participants analyze the Lorentz transformation and the implications of four-velocity, noting that the same values for time in both frames seem incorrect. They clarify that the distance to Titan should be length contracted in the spacecraft frame, and velocities must be equal and opposite between frames. Ultimately, the time measured in the spacecraft frame is half that of the inertial frame, and a spacetime diagram is proposed to illustrate the scenario.
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Homework Statement
An inertial observer O ' in a spacecraft, moving with four-speed U = 2 (c, u) seen by a
Earth observer O, passes by Earth and synchronizes his clock with O's clock. This
observer turns to Titan, a moon of Saturn that is (at that time) at a distance
Δx = 1.2 billion km from Earth.
How long does that observer take to reach Titan as seen from Earth? And measured by
the same? How far is the land of Titan seen by O '?
Relevant Equations
Lorentz transformation
I get the same values for both observers, which is not nice I think.
 
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pepediaz said:
Homework Statement:: An inertial observer O ' in a spacecraft , moving with four-speed U = 2 (c, u) seen by a
Earth observer O, passes by Earth and synchronizes his clock with O's clock. This
observer turns to Titan, a moon of Saturn that is (at that time) at a distance
Δx = 1.2 billion km from Earth.
How long does that observer take to reach Titan as seen from Earth? And measured by
the same? How far is the land of Titan seen by O '?
Relevant Equations:: Lorentz transformation

I get the same values for both observers, which is not nice I think.
Yes, that doesn't sound right. Please post what you did.
 
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Be ϒ the Lorentz transformation:

Δx/U = Δx /(2cc-2uu) = t
Δx'/U' = ϒΔx /ϒ(2cc-2uu) = t'

Thus, t=t'
 
pepediaz said:
Be ϒ the Lorentz transformation:

Δx/U = Δx /(2cc-2uu) = t
Δx'/U' = ϒΔx /ϒ(2cc-2uu) = t'

Thus, t=t'

That's hard to read and difficult to understand. Can you explain what you're doing?

First, what does ##U = 2(c, u)## mean?
 
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I'm calculating the time for each observer. U is the four-velocity, and I have expressed it in form of invariant product (as an absolute value, but with a "-" between squared components).

For the observer inside the spaceship, I have considered that their distance and velocity is that of the inertial observer, but multiplied by the Lorentz factor, I think that's wrong, but I don't know how to do it different.
 
pepediaz said:
I'm calculating the time for each observer. U is the four-velocity, and I have expressed it in form of invariant product (as an absolute value, but with a "-" between squared components).

For the observer inside the spaceship, I have considered that their distance and velocity is that of the inertial observer, but multiplied by the Lorentz factor, I think that's wrong, but I don't know how to do it different.
Sorry, none of this makes much sense. Let me repeat the question you didn't answer:

PeroK said:
First, what does ##U = 2(c, u)## mean?
 
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U is the four-velocity, and it has a temporal component (c) and three space-coordinate components(u, as a vector).
 
pepediaz said:
U is the four-velocity, and it has a temporal component (c) and three space-coordinate components(u, as a vector).
What is the ##2##?
 
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I guess it is a coefficient, but I'm not sure.
 
  • #10
pepediaz said:
I guess it is a coefficient, but I'm not sure.
Isn't that a problem?

What is the general form of a four-velocity? Hint: think about the gamma factor ##\gamma##.
 
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  • #11
\mathbf {U} =\gamma (c,{\vec {u}})=(\gamma c,\gamma {\vec {u}})


So, I can obtain inertial velocity equating γ=2.

Once done this, I continue having the same problem:

t = Δx /v, but t' = Δx '/v' = γ(Δx)/γ(v)
 
  • #12
pepediaz said:
\mathbf {U} =\gamma (c,{\vec {u}})=(\gamma c,\gamma {\vec {u}})


So, I can obtain inertial velocity equating γ=2.

Once done this, I continue having the same problem:

t = Δx /v, but t' = Δx '/v' = γ(Δx)/γ(v)

Okay, so you have ##\gamma = 2##. That gives you ##u##, if you need it. And in the Earth frame, we have ##t = \frac{\Delta x}{u}##.

In the spacecraft frame, what do we have?
 
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  • #13
I guess t' = Δx '/v' = γ(Δx)/v
 
  • #14
pepediaz said:
I guess t' = Δx '/v' = γ(Δx)/v
How far is Titan from Earth in the spacecraft frame?

How fast is Titan moving in the spacecraft frame?
 
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  • #15
In the spacecraft frame, the distance would be γ(Δx) and the velocity would be v, or γ(v), this one I don't know.
 
  • #16
pepediaz said:
In the spacecraft frame, the distance would be γ(Δx) and the velocity would be v, or γ(v), this one I don't know.

That's not correct. The distance to Titan is length contracted. And, velocities must be equal and opposite between frames. If the rocket is moving at speed ##u## in the Earth frame, then the Earth and Titan must be moving at speed ##u## in the spacecraft frame.
 
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  • #17
I understand it now! Thanks!

The time in spacecraft frame is a half of the inertial frame time.
 
  • #18
And another thing, be the red point this spacecraft , the purple line the world line with slope = 2 and the green point a photon thrown towards the Earth from the spacecraft , would this spacetime diagram ok? (distance would be 1.2 billion km, and the time, 1000 times of shown, but scale is badly displayed, even the red point wouldn't be at that position, but I did it like this just for showing it).

2020-05-11.png
 

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