Pete,
Okay, let's try to apply Lorentz transformation for the exercise I gave to depict MacM's wrong view.
Applying LT for spaceship passing earth event gives us t=t'=0 and x=x'=0.
Now, apply LT for t=2 seconds and x=0 that is an event occuring on earth at the time the spaceship arrives to the moon. This is the result:
You can verify using other method that event at D occurs at t=0 in earth reference frame and event at E occurs at t=2sec in earth reference frame, say, by first synchronize clocks at D and E to ensure that they both tick simultaneously.
Pete said:The task as I understand it is to determine the transit time of the beam in the spaceship frame.
To me, this means determining the time difference between points A and B.
Yes, these points are in different places in the spaceship frame - and that's OK. (see note below)
Okay, let's try to apply Lorentz transformation for the exercise I gave to depict MacM's wrong view.
Say, you are in a spaceship moving at v=0.6c from earth to moon. If earth-moon distance is 1.2c second, according to earth observer you need (1.2c second)/0.6c=2 seconds to reach moon. Now, from your point of view. You see earth-moon distance as 0.8*1.2c second = 0.96c second. According to MacM's interpretaion, you still need 2 second (instead of 1.6second suggested by standard SR) to complete the trip and therefore you will find that your velocity relative to earth (or moon) is (0.96c second)/2 = 0.48c. This cannot be right (Correct only based on MacM's relativity, which is the wrong version of relativity).Based on standard SR you will still see the relative velocity as (0.96c second)/1.6 = 0.6c! There is nothing to talk about on MacM's view on this matter, seriously, because his view is WRONG.
I believe you agree that for this case, the spaceship observer measures the time for the trip as 1.6 second and the earth-moon distance as 0.96c second, while earth observer measures them as 2 second and 1.2c second respectively. Applying LT for spaceship passing earth event gives us t=t'=0 and x=x'=0.
Now, apply LT for t=2 seconds and x=0 that is an event occuring on earth at the time the spaceship arrives to the moon. This is the result:
x' = 1.25*(0-0.6c*2) = 1.5c second
t' = 1.25*(2-0) = 2.5 second
Next, apply LT for t=2 seconds and x=1.2c second that is an event occuring on the moon at the time the spaceship arrives to the moon. This is the result: t' = 1.25*(2-0) = 2.5 second
x' = 1.25*(1.2c-0.6c*2) = 0
t' = 1.25*(2-0.6*1.2) = 1.6 second
You can see that the correct result is obtained by applying LT for the spaceship arriving the moon event, which occurs at x'=0 at the same position as the spaceship passes earth event. The distance covered by the spaceship during the 1.6 second trip, according to the spaceship observer, is 0.6c*1.6 = 0.96c second. t' = 1.25*(2-0.6*1.2) = 1.6 second
Pete said:Your interpretation of the problem is that it means determining the time interval separating points D and E, right?
The reason I don't like that is that in the spaceship frame, point D isn't simultaneous with the beam leaving Earth, and point E isn't simultaenous with the beam returning... so to me it doesn't seem meaningful to consider that interval to be the spaceship's observation of the transit time.
You can verify using other method that event at D occurs at t=0 in earth reference frame and event at E occurs at t=2sec in earth reference frame, say, by first synchronize clocks at D and E to ensure that they both tick simultaneously.