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Most silicon photovoltaic arrays on Earth are silicon (no layers of III-V material for added efficiency) and they are grown as polycrystalline silicon rather than sliced from single crystal silicon lowering the cost substantially.

Answer(s) to Why does the ISS not use the most efficient solar panels available? tell us that the ISS' original panels are single junction silicon rather than dual or triple junction stacks for reasons of weight.

The ease of breakage of the individual elements in the original arrays described in this answer to How are the silicon PV cells constructed in the ISS's solar panels? Are they as flexible as they appear here? suggest they are polycrystalline silicon (a good silicon wafer without scratches is surprisingly durable) but it's not yet definitively established.

My guess is that for practical reasons both original and ROSA silicon will be polycrystalline, which is far cheaper to manufacture than thin single crystal, but so far I don't have a source that establishes this with certainty.

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The ISS solar cells are Spectrolab K-6700B wrapthru solar cells that come in a couple different versions. They are monocrystalline, bifacial, single junction silicon cells, which were more or less state of the art when they were specced out for the space station power system, which was roughly in 1989.

The ISS IROSA cells are Spectrolab XTJ Prime cells, which (I believe) are monocrystalline, triple junction GaInP/GaAs/Ge cells.

For space applications, cost is far less important than reliability (indeed, the cells, though expensive for your or my pockets, are only a fraction of the integration cost of a project that uses them).

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  • $\begingroup$ Thanks for your speedy answer! Now that I look again, with the four sawed sides and through holes yes I'd expect they would be quite breakable compared to new wafers straight out of the box. $\endgroup$
    – uhoh
    Commented Oct 7, 2021 at 6:31

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