Quote:
Originally Posted by the-red-scare
I know Spaceships doesn’t concern itself with these things. If it did, I wouldn’t need to ask about them. But I concern myself with these things, hence the question.
So does anyone know if rocket cross-sectional area should scale with mass flow rate?
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Nozzle area mostly scales with mass flow rate (with some variance based on design) but this isn't a significant limiting factor for most rockets we actually deal with in the real world.