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Fig.4
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In the following we assume the interstellar field as orientated perpendicular to the direction Sun-Epsilon Eridani to simplify the scenario.
In Sec.3.3 (Braking) we shall see that the decelerating phase (Stage 4) takes as long as the accelerating phase (Stage 1). If we assume constant acceleration and deceleration, the distance d between Sun and Epsilon Eridani is as same length as the distance of the force-free flight (the green line).
In the last section we already determined the initial velocity at Stage 2 to (see above):

After having been accelerated, our ship overcomes the distance of ten light-years in

Here we see: It must be guaranteed that our brave space pioneers can overcome such a long period in isolation - but this is another theme. Nevertheless, let us concentrate on Stage 3.
To describe the turning we remember the definition of the angular velocity
B , see also (2b.01) ...
(3b.01)
... and the relationship we discovered in Chap.2, Sec.2.1 (go to):
(3b.02)
We realize: the angular velocity depends on the electric charge Q and the mass m of the body - as well as on the magnetic induction B0. First of all we are interested in the Period TC of a complete circulation. Please keep in mind that our ship carry out only a part of this circulation. If we equalize both formulas (3b.01) (3b.02), we have:
(3b.03)
How strong is the interstellar magnetic field?
According to Forward, it has a strength of B0 = 3 . 10-5 g = 3 . 10-9 T [Forward (1964)]. Perhaps this is a bit too optimistic; therefore we would like to refer to newer sources [Musser (2000)], in which a field strength of B0 = 5 . 10-10 T is given. The next interesting question concerning the ship is: how strong could we charge it up?
Here we have the problem, that the properties of the interstellar matter are not well known. Ionized gas particles could - once the ship is charged - be attracted and captured by the ship's stripes. Thus, the generators on board must compensate this neutralizing effects. We assume that the inert atomic nuclei of the (possible) ionized interstellar gas are not as strong attracted by the ship as the lighter electrons. Therefore we want our ship be charged negatively, perhaps in future it is possible to generate a charge of Q = - 1010 C.
By the way, we have an additional problem (but here we cannot go into the details): While traveling with relativistic speeds, crew and equipment are being exposed to a high cosmic radiation.
In the previous section we took a ship mass of m' = 7.58 . 107 Kg. According to formula (3b.02) we are now able to calculate the angular velocity of the turning to

With this result, our ship needs for one circulation a time TC of:

With the radius R of the circulation and the angular
(see Fig.4) we can calculate the duration T of the turning (Stage 3). To find out the radius R we refer to equation (2b.02):


Therefore we have:

According to Fig.4, tan(
/2) is given by

This means an angular of
= 2.86o.
With a few trigonometric calculus and the circulation period TC we can easily derive the duration T of the turning phase. Here we intent you to calculate the relationship between those periods. Our result:
(3b.04)
If we insert the period TC into this equation, we get a period of about T = 1.52 a.
Finally, we calculate the length of phase 3 (the blue line in Fig.4) to:
s = v.T = 0.54 c . 1.52 a
0.82 ly ,
referring to a length of nearly s = 7.76 . 1015 m.
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Chapter Three