They do scale down further than liquids. Ullage and stage separation motors, kick motors to give a hundred m/s or so to a small satellite...they're just a grotesquely inefficient thing to use for any substantial part of the overall delta-v budget. The long chain of hazardous material handling requirements and many opportunities for a catastrophic failure if a tiny fault is missed are other reasons for keeping solids small.
And I see not a word from Jerry to address what he quoted from my post. Why must we use hazardous, inflexible, unscalable, poor-performing solid rockets to get men to Mars?




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