In addition to prepping the TR-1 motor for another test I will be doing some smaller scale testing utilizing Dextrose. I plan to use the 2.375" motor that designed, tested, and flew back in 2009/10.
Originally this motor was designed for sorbitol based propellant. Ultimately it was fired with KNSB based propellant and a 50/50 sorbitol/Erythitol mix based propellant. I have constructed a four segment casing for this motor which would produce a low MEOP of 600psi with KNSB and 950psi with KNDX.
|SRM screen grab|