updated index

[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..fd26ef056a0a40187e8fedee5ae72a3450f078ad 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-->
@@ -20,4 +20,7 @@ Total of 110.8g propellant, vs 122g simulated.
 
 ## Results ##
 
+Flown in Robert's Madcow Little John at NCR's Mile High Mayhem on 3 June 2017,
+PFND.  Used two Twiggy igniters wired in parallel.
+
 Flight data logged as ? sn ?, flight ?.