X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=blobdiff_plain;f=rockets%2Fresearch%2F2020-batch-01.mdwn;fp=rockets%2Fresearch%2F2020-batch-01.mdwn;h=0000000000000000000000000000000000000000;hp=f66091a0e689300f9c8aed0215c01426cff32606;hb=8b5b14fb20cbc68313427127532a8241c920a586;hpb=7357678e1fb78cfbd42b39c882b114a1ca5a95f6 diff --git a/rockets/research/2020-batch-01.mdwn b/rockets/research/2020-batch-01.mdwn deleted file mode 100755 index f66091a..0000000 --- a/rockets/research/2020-batch-01.mdwn +++ /dev/null @@ -1,56 +0,0 @@ -# Batch 2020-batch-01 # - -8 grains of 75mm KNSB, intended to be a reload for my long purple case. -with Loki-style #58 nozzle. Grain length 5.125" with 0.125" spacing per -grain planned using o-rings. Delrin coring rods of 0.75" diameter since -that's what I have bases and caps for, then bored out to 0.875" final ID -before assembly. - -Kuker's Motorsim says this should be a 43% M-2690 with a slightly progressive -burn about 2.5 seconds long, using 5355g of propellant or 73% volume loading, -and a max pressure of 825 psi. - -Since this is too much propellant to handle in one batch, we'll plan to use -two 2700g batches, the formula for each of which is: - -* 65% KNO3, 1755g -* 35% Sorbitol, 945g -* 1% red iron oxide, 27g, added after melt -* 41 drops Polystep-B1, added before pour using eye dropper - -This formula is completely fluid with 225F indicated on the Presto Multicooker, -but viscosity is noticeabley lower making for easier pouring at 250-275F. - -These grains were cast on 2020.08.31. - -## Results ## - -The 5.125" grains were poured to a 119mm fill line, and then an 0.75" Delrin -coring rod was twisted down into the goo puncturing foil over the coring rod -hole at the grain base. About 18 hours later, the grains were "topped off" -and smoothed level to compensate for shrinkage. The coring rods were pulled -about 48 hours after casting, and each grain was observed to have some bubbling -around the base of the coring rod, presumed to be due to air below the foil on -the casting base pushing up as the rod went down. We should arrange for -explicit venting of that in the future. The top faces of the grains were knife -scraped smooth, the cores were bored out to 0.875", and the bottom of each grain -was chamfered around the core to eliminate the bubbly bits. Thus, the grain -masses were highly likely to be less than anticipated. - -* Grain 1, 630g gross, 16.21g casting tube, 613.79g net -* Grain 2, 634g gross, 16.20g casting tube, 617.80g net -* Grain 3, 640g gross, 16.14g casting tube, 623.86g net -* Grain 4, 632g gross, 16.17g casting tube, 615.83g net -* Grain 5, 626g gross, 16.34g casting tube, 609.66g net -* Grain 6, 628g gross, 16.11g casting tube, 611.89g net -* Grain 7, 628g gross, 16.17g casting tube, 611.83g net -* Grain 8, 636g gross, 16.28g casting tube, 619.72g net - -Average casting tube weight 16.2g. Measured total propellant mass of 4924g, -or about 616g per grain, which is 92% of what Kuker's simulator projected. - -Borrowed Terry's Loke #58 nozzle, which is a few thousandths over-sized. - -The as-built motor is projected to be a 30% M-2300 or so. - -Flight attempted at Airfest 2020 on Monday morning, CATO just off the rail.