Use the Minkowski metric with signature and write , . Future-pointing timelike means and . Thus
so is again future-pointing timelike.
Let and . In a Lorentz frame where , the future-pointing vector has . Consequently , with equality exactly when has no spatial component in that frame. Hence
Taking positive square roots proves
Equality holds exactly when are positive scalar multiples of each other. This is the reverse triangle inequality for future timelike vectors, not the Euclidean triangle inequality.
Take spacetime coordinates . Differentiating the initial segment gives the four-velocity
The identity gives , and . The proper time element therefore satisfies , with the future orientation selecting . Thus is proper time along this path.
Since is proper time, the four-acceleration is
Its Minkowski norm squared is , so the invariant magnitude of proper acceleration is
The vector is spacelike, which accounts for the minus sign under the square root.
Differentiate each segment and express the four-velocity using a continuous rapidity:
At both rapidities are ; at both are . Hence the four-velocity is continuous at both junctions. This expression also gives everywhere, so the parameter remains proper time on the later segments.
Away from the junctions,
with successively . The rapidity is continuous but its slope reverses. Thus the four-acceleration has a finite jump to its negative at each junction, while its magnitude stays on either side. There is no velocity jump; the idealized path is continuously differentiable but not twice differentiable at the switching events.
At and , the mission is at the planet's position . The final coordinate time from the last segment is
The planet is at rest in these coordinates, so its proper time elapsed equals this coordinate-time difference. The astronauts' proper time is the parameter interval, . Therefore
For proper acceleration and , seconds, approximately one year. Thus and . Neglecting in the hyperbolic sine,
The clocks compare two different timelike paths between the same departure and reunion events.
Put . At emission, , the middle segment gives
The planet is at , so the inward light signal takes coordinate time
Its arrival time on the planet is therefore . Subtract this from the mission's return time :
For large at fixed acceleration this tends to . With the Earth-gravity value above, the wait is approximately two years, despite the millions of planet-years elapsed since departure in part (i).
Figure 1.
An accelerated round trip and the midpoint signal received before reunion
. Original spacetime diagram at omega T=1.2 for visibility. The planet follows the vertical line. The mission sends an inward light signal from its most distant point; the signal reaches the planet before the final reunion. Both axes use the same dimensionless spacetime scale. Details.

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