Recent time, some projects to launch spacecraft to the nearest star have been proposed. Since such a spacecraft should be accelerated to subluminal velocities and since no one engine is able to accelerate the apparatus to the needed velocities, the only realistic way is to use the sail as a unit to get the accelerated force for the spacecraft . It is assumed that the sail is the perfect mirror illuminated by the powerful laser beam located in the Earth's orbit.
Thee are some works where the parameters of the mirror are analyzed. What is important that in all these works, the parameters of the mirror do not change with the velocity and it allows to make some calculations of the (assumed) flight of the spacecraft.
But let us consider if it is so.
When this apparatus with the mirror begins to fly with constant velocity (the beam does not illuminate the mirror) this system seems to be considered as an inertial frame. At least an observer being in the spacecraft can treat is in this way.
But one question arises, namely, if the reflection coefficient of the mirror is the same in two frames, the frame of the laser (the Solar system) and the frame of the spacecraft.
The reflection coefficient Rc depends on the electroconductivity \sigma of the metallic layer of the mirror - the higher the \sigma, the better the Rc. The parameter \sigma is determined with good accuracy by the formula (Eq. 7.58 of Jackson's Electrodynamics) (in latex)
\[
\sigma=(f*Ne^2) / (m \gamma)
\]
where m is the mass of electron, f*N the number of free electrons per unit volume in the medium, the damping coefficient \gamma is determined by perfectness of the material (defects, impurities etc).
All parameters in the formula don't depend on the velocity. But the masses of the electrons of conductivity depend on the velocity of the mirror (they co-move with the mirror) as
m= m_0/\sqrt{1 - (v/c)^2}.
It means that the electroconductivity and therefore Rc will be different in different frames - according to the observer in the Earth, Rc decreases with increase of the velocity. In the frame of the spacecraft, Rc is the same as before acceleration.
Thus, we have two inertial frames. But these frames are not equivalent since the electrons should have different masses (the increase of the electron masses was still confirmed by experiments of Kaufmann).
How to resolve this contradiction of the special relativity?
PS. The mechanism of change of \sigma and Rc is described in detail in my E-print:
https://www.researchgate.net/publication/389314847_Comment_on_work_of_Umrigar_and_Anderson_Energy_needed_to_propel_a_tiny_spacecraft_to_Proxima_Centauri_and_an_unstated_assumption_in_Einstein's_1905_paper_arXiv250204331v1
But all that I explained above is sufficient to describe the problem with non-equivalence of the frames.