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Isn't one of the advantages of the hybrid solid fuel / liquid oxidizer design that it can be throttled to some extent by cutting off the oxidizer using a valve?

I do agree that I can't see why a feather during a burn would ever be desired, but we'll have to wait for the NTSB to see whether the flaw was in the design or manufacture.



Yep, you're right. I was confusing the SS2 design with the shuttle SRBs. My mistake.




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