update test files with simulation plots, etc

[web/gag.com] / rockets / research / 2017-test-06.mdwn

diff --git a/rockets/research/2017-test-06.mdwn b/rockets/research/2017-test-06.mdwn
index a3b95dc4fac4a5340a5829e425b87db4cd785704..4c656083411552caa3e25d9cc991788f12811c3a 100755 (executable)
--- a/rockets/research/2017-test-06.mdwn
+++ b/rockets/research/2017-test-06.mdwn
@@ -1,9 +1,9 @@
-# Test 2017-05 #
+# Test 2017-06 #
 
 4 grain 29mm sorbitol motor 
 
 With a 7.40" liner, 14/64" nozzle throat, buna-n o-rings, simulation says
-this reload will be a 99% G-180, 159 Ns, with about an 0.8 sec burn.
+this reload will be a 99% G-180, 159 Ns, with about an 0.8 sec burn:
 
 <p>
 <!--Begin motor 29mm 4-grain Sorbitol #14 HTML export from MotorSim-->