1) Given x' = 1/a (x - vt) and t' = 1/a (t - vx/c2),
Then: x' = x/a - vt/a and t' = t/a - vx/ac2
and: x' + vt/a = x/a and t' + vx/ ac2 = t/a
so:
x = a(x' + vt/a) and t' = a(t' + vx/ ac2 )
finally: x = a(x' + vt) and t = a(t' + vx/c2)
2) We have: x' = 60m, t' = 8 x 10-8 s and y' = y, z' = z
v = 0.6c = 1.8 x 108 m/s
Then:
x = [60m + (1.8 x 108 m/s)( 8 x 10-8 s)]/ (0.64)½
x = [60m + 14.4m]/ 0.8 = 74.4m/0.8 = 93m
and t =
[(8
x 10-8 s)+ (1.8 x 108 ms-1)(60m)/(3 x 108
ms-1)2/0.8
t = 2.5 x 10-7 s/ 0.8 = 2.33 x 10-7 s
The space time coordinates are: (93 m, 2.33 x 10-7 s)
3) The problem requires no relative motion defined specifically in the x-direction so the equations:
t = t' + x'v/c2/(1 - v2/c2)½
and
t' = t - xv/c2/(1 - v2/c2)½
are immediately simplified by the terms in x becoming zero, so:
t = t'/(1 - v2/c2)½
and
t' = t /(1 - v2/c2)½
Here: t = time passage on Earth clock
and t' = time passage on astronaut's clock
For t = 1 Earth year = 365 ¼ days:
t' = (365 ¼ days)/ [1 - (0.9c)2/c2]½
t = 2.5 x 10-7 s/ 0.8 = 2.33 x 10-7 s
The space time coordinates are: (93 m, 2.33 x 10-7 s)
3) The problem requires no relative motion defined specifically in the x-direction so the equations:
t = t' + x'v/c2/(1 - v2/c2)½
and
t' = t - xv/c2/(1 - v2/c2)½
are immediately simplified by the terms in x becoming zero, so:
t = t'/(1 - v2/c2)½
and
t' = t /(1 - v2/c2)½
Here: t = time passage on Earth clock
and t' = time passage on astronaut's clock
For t = 1 Earth year = 365 ¼ days:
t' = (365 ¼ days)/ [1 - (0.9c)2/c2]½
=
(365 ¼ days)/(1 - 0.81)½
t' = (365 ¼ days)/0.436 = 837.7 days
t' = (365 ¼ days)/0.436 = 837.7 days
This is the time elapsed on the astronaut's clock when the Earth has made one revolution equal to 365 ¼ days. In other words, each of his days is roughly equal to 2.29 Earth days. Hence, his clock is obviously running slower than the Earth clock.
A more intuitive way to look at the result would be in terms of the time transformation:
t
= t'/ (1 - v2/c2)½
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