From: Bdale Garbee <bdale@gag.com>
Date: Sat, 7 Oct 2017 16:25:27 +0000 (-0600)
Subject: capture grain batch numbers
X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=commitdiff_plain;h=05222e7c72a1d45c60e96d3dd8fa1865af2a0b35;hp=f165298afe00182b962ed7fb5b1d806f542e6cec

capture grain batch numbers
---

diff --git a/rockets/research/2017-test-12.mdwn b/rockets/research/2017-test-12.mdwn
index 24ebc6a..69cf885 100755
--- a/rockets/research/2017-test-12.mdwn
+++ b/rockets/research/2017-test-12.mdwn
@@ -21,11 +21,11 @@ Simulation says this is a 57% L-1366 with 3804 Ns total impulse, 797 psi max,
 Neglected to re-weigh grains after trimming and before epoxying into the 
 liner.  These were the pre-trim masses:
 
-* Grain 1, 590g gross, 574g net, trimmed to 4.5" long
-* Grain 2, 594g gross, 578g net, trimmed to 4.5" long
-* Grain 3, 592g gross, 576g net, trimmed to 4.5" long
-* Grain 4, 584g gross, 568g net, trimmed to 4.4375" long
-* Grain 5, 580g gross, 564g net, cut to 4" long
+* Grain 2017-7-1, 590g gross, 574g net, trimmed to 4.5" long
+* Grain 2017-7-2, 594g gross, 578g net, trimmed to 4.5" long
+* Grain 2017-7-3, 592g gross, 576g net, trimmed to 4.5" long
+* Grain 2017-7-4, 584g gross, 568g net, trimmed to 4.4375" long
+* Grain 2017-7-5, 580g gross, 564g net, cut to 4" long
 
 Total propellant load thus somewhat less than 2860g.