Don’t know if anyone would find it useful, especially in a 5yr old thread, but I finally found some more in-depth info relating to the Sprint or
HiBEX propellant (ultra high burn rate stuff). It’s more or less the same propellant used in the Russian ABM system by the looks of it. 12” per
second at 2000psi with a CMDB.
https://apps.dtic.mil/sti/tr/pdf/AD0530958.pdf
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