</p>
Neglected to re-weigh grains after trimming and before epoxying into the
-liner.
+liner. These were the pre-trim masses:
-* Grain , g gross, g net, 4.5" long
-* Grain , g gross, g net, 4.5" long
-* Grain , g gross, g net, 4.5" long
-* Grain , g gross, g net, 4.4375" long
-* Grain , g gross, g net, 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 of g propellant, vs g simulated.
+Total propellant load thus somewhat less than 2860g.
## Results ##
O-rings made forward closure a *very* snug fit.
-Flight data logged as ? sn ?, flight ?.
+Flight data logged as sn 3121, flight 3 on 2017-10-08. 8353 ft apogee, Mach 0.7, 3.4 sec boost.
+