Tiago said:
Don't worry, it's probably me that's not explaining myself in the best way. My point was, if the Earth is traveling at different speeds according to different IRF's, it also means that it's traveling at different % of c.
Yes, that's true but the fact that you are stating this makes me wonder if you really understand what it means. Specifying a speed as a percentage of c does not imply anything about an IRF. It's just a conversion factor. We could have also specified 10%c as 29979.2458 kilometers per second which has no reference to the speed of light.
Tiago said:
According to the Sun it might be traveling at 10% the speed of light, according to Jupiter it might be at 12%c, and so on.
If the Earth is traveling at 10%c according to the sun, then the sun is traveling at 10%c in the opposite direction according to the earth, correct? I still don't know why you want to include the sun or Jupiter in a scenario that is fundamentally about a rocket taking a trip at some speed with respect to the earth.
Tiago said:
So when we say that our rocket is traveling at 99%c, it also means that it can travel at 99%c according to the Earth,
No, it doesn't mean that unless you specifically say so. When you set up a scenario, it is your responsibility to specify all the details. If you want the rocket to travel at 99%c with respect to the earth, then you have to say so. You can't just say that it is traveling at 99%c and leave it up to us to guess that you meant with respect to the earth.
Tiago said:
but according to the Sun it might traveling at 80%c.
Even if you meant that the rocket is traveling at 99%c with respect to the Earth and the sun is traveling at 10%c with respect to the earth, you can't just say that the rocket is traveling at 80%c (or some other speed) according to the sun. The problem is that since the rocket spends the first part of its time traveling
away from the sun (and the earth) and the last part of its time traveling back
towards the sun (and the earth), there has to be at least two different speeds that the rocket is traveling according to the sun. The first speed will be slightly less than 99%c and the last speed will be slightly more than 99%c. You have to use the
velocity addition formula to determine what these speeds are. I'll show you how to do that later.
Tiago said:
And this should mean that we're "travelling in time" according to Earth, but not according to the Sun, right?
No, that's not right. In fact, the difference between the amount of aging that goes on during the trip for the Earth and the sun is only 10%. I'll show that later also.
Tiago said:
(cause 80% is not significant) Hope I got this right, but please don't worry if I didn't :) I really thank everyone's effort in sharing their knowledge to educate people like me who don't have the proper basics in physics but love the area and are fascinated by it. Wish I could go back and take a course in physics, cause there are things that are easier to learn with teachers than just reading from wiki articles :)
Let me show you some spacetime diagrams to illustrate the concepts that you have been raising in this thread. We'll start with the rest frame of the Earth and with the sun traveling at 10%c. The rocket travels at 99%c for 5 years, then turns around for another 5 years to get back to earth. The dots mark off one-year increments of time for each object:
As you can see, the Earth has aged 71 years compared to 10 years on the rocket when they meet. But the sun has aged 64 years by the time it meets up with the rocket which is not the huge difference you expected. Note that the Time Dilation of the rocket is the same during both halves of its trip according to the IRF in which the Earth is at rest.
Now we can use the Lorentz Transformation process to see what this scenario looks like in the rest frame of the sun:
Although the Lorentz Transformation automatically determines all the details of all the objects, it might be a little hard to see the actual speeds of the rocket during both parts of its trip. We can use the velocity addition formula for this purpose. For velocities that are fractions of the speed of light where c=1, it looks like this:
s = (v+u)/(1+vu)
For the situation where the rocket is traveling in the same direction as the sun, we have to set v = 0.99 and u = -0.1:
s = (v+u)/(1+vu) = (0.99-0.1)/(1+(0.99)(-0.1)) = (0.89)/(1-0.099) = (0.89)/(0.901) = 0.98779
And for the return part of the trip, we set v = 0.99 and u = 0.1:
s = (v+u)/(1+vu) = (0.99+0.1)/(1+(0.99)(0.1)) = (1.09)/(1+0.099) = (1.09)/(1.099) = 0.99181
As you can see, in the IRF of the sun, there is very little difference between the speeds of the rocket in the two directions. It may be difficult to see the difference in their Time Dilations but it is just enough to make the Proper Times as marked by the dots come out the same in this IRF as it did in the original IRF, that is, the respective agings of the objects when they meet are identical.
Just for the fun of it, I have made another pair of diagrams for a different scenario where instead of the sun traveling at 10%c with respect to the earth, I'm having Saturn travel at 66%c with respect to the Earth to make the differences between the red object and the other objects more apparent:
The relationships between the rocket and the Earth are the same as in your scenario but there is a big difference between Saturn and the sun. Saturn ages by only 32 years when it meets up with the rocket. Note that a big part of this difference is due to the larger Time Dilation of Saturn compared to the sun. Remember, Time Dilation increases with speed.
But now we can transform to the IRF of Saturn:
Now you can easily see a difference in the Time Dilations of the rocket during each part of its trip.
Any questions?