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[web/gag.com]
/
rockets
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research
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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 2017-0
5
#
+# Test 2017-0
6
#
4 grain 29mm sorbitol motor
With a 7.40" liner, 14/64" nozzle throat, buna-n o-rings, simulation says
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-->
<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 ##
## 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 ?.
Flight data logged as ? sn ?, flight ?.