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SRBs as Nozzles & Segments


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Interesting idea - actually being able to adjust the burn speed for each segment could be used to change the flight profile (for example adjusting a lower energy burn for the segment corresponding to MaxQ).

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On one hand, I like the idea of making solid rockets more like liquid rockets with a more modular system that lets you tailor how much booster you want.

On the other hand, how much detail do you want? Would it behave exactly like liquid fuel rockets with more solid fuel = more delta-V but fixed thrust, or more segments = more thrust with the same burn time as for real SRBs? Are we including fuel shaping to control the rate of combustion and so the thrust curve, and is that on a per-segment basis or controlled by the nozzle for the whole booster?

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