X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=blobdiff_plain;f=rockets%2Fresearch%2F2019.11.23.mdwn;fp=rockets%2Fresearch%2F2019.11.23.mdwn;h=e72528edb7eb7c4369a36ed9d4fc09b54ea67509;hp=0000000000000000000000000000000000000000;hb=62f21674407be0fde2761f6a39117b4cfe95eb00;hpb=48636f735a4e18224378c4bdcc9118d0d533a65e diff --git a/rockets/research/2019.11.23.mdwn b/rockets/research/2019.11.23.mdwn new file mode 100755 index 0000000..e72528e --- /dev/null +++ b/rockets/research/2019.11.23.mdwn @@ -0,0 +1,33 @@ +# Batch 2019.11.23 # + +A solid slug of KNSB propellant cast in PML 75mm coupler tube, intended to be +cut into 1" long grains to be used in James' ballistic test motor. For +6 grains, thinking about saw kerfs and shrinkage, we'll try casting about a 7" +length. That calculates to about 1321g. + +After trying with and without RIO last year, then losing the notes on which +tests were which, I'm kind of starting over. For prior with-RIO motors, I +used 1% RIO and about 1.5 drops per 100g of Polystep-B1 surfactant. At this +motor size, I don't think the surfactant is useful, but I do think some RIO +helped with igniteability. So this time, let's try running with less RIO +and no surfactant. Like 0.25% RIO. + +Formula for a batch size of 1325g: + +* KNO3, 859.10g +* Sorbitol, 462.59g +* red iron oxide, 3.31g + +This formula is completely fluid with 225F indicated on the Presto Multicooker. + +## Results ## + +These grains were cast on 23 November 2019, in the wee hours. + +The actual measures of the batch (using shipping scale for primary ingredients +and my 0.01g resolution scale for the RIO) were: + +* KNO3, 860g +* Sorbitol, 462g +* red iron oxide, 3.4g +