add flight stats

[web/gag.com] / rockets / research / test5.mdwn

diff --git a/rockets/research/test5.mdwn b/rockets/research/test5.mdwn
index 4f2a59c6d642087c27ae8cdae8ed2ba220845e64..d6367784f391ef12485de4e1ace91b0039a22ac3 100755 (executable)
--- a/rockets/research/test5.mdwn
+++ b/rockets/research/test5.mdwn
@@ -4,10 +4,10 @@ Trying again using KNSO with our new casting bases.  We also have a real
 eye-dropper now for measuring the surfactant.  4 38mm grains of 
 1.875" length, 250 gram batch using formula of
 
-* 65% KNO3
-* 35% Sorbitol
-* 1% red iron oxide
-* 3 drops Polystep-B1 (1 drop per 100g being the general idea)
+* 65% KNO3, 162.5g
+* 35% Sorbitol, 87.5g
+* 1% red iron oxide, 2.5g, added after melt
+* 3 drops Polystep-B1, added before pour
 
 ## Process ##
 
@@ -97,4 +97,6 @@ seconds after coming up to pressure.  The regressive curve seems a bit
 exagerated in the flight accel data, which seems completely explainable by
 the nozzle throat erosion causing pressure to faill during that period.
 
-Pretty cool for our first real flight test!
+The airframe saw an average of 12 G acceleration on the way to Mach 0.6 and
+2838 feet above the laucnh site which is at 8800 feet MSL.  Perfect 
+recovery!  Pretty cool for our first real flight test!