X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=blobdiff_plain;f=rockets%2Fresearch%2F2017-batch-03.mdwn;h=b390854c016cf0344da0774710ff89edcf37208a;hp=316d4400100254426244de925de5bf42a7a548ee;hb=c3209ea421e038c69530f8f7e085d842dc212eda;hpb=26136930d2b4b2cd57821aa3e730c925f2616678

diff --git a/rockets/research/2017-batch-03.mdwn b/rockets/research/2017-batch-03.mdwn
index 316d440..b390854 100755
--- a/rockets/research/2017-batch-03.mdwn
+++ b/rockets/research/2017-batch-03.mdwn
@@ -18,12 +18,12 @@ Liner should be cut to 10.00" long for this 6-grain reload.
 
 ## Results ##
 
-* Grain 1, 176.1g gross, ?g net
-* Grain 2, 187.8g gross, ?g net
-* Grain 3, 187.6g gross, ?g net
-* Grain 4, 185.8g gross, ?g net
-* Grain 5, 187.9g gross, ?g net
-* Grain 6, 188.3g gross, ?g net
+* Grain 1, ?g gross, ?g net
+* Grain 2, ?g gross, ?g net
+* Grain 3, ?g gross, ?g net
+* Grain 4, ?g gross, ?g net
+* Grain 5, ?g gross, ?g net
+* Grain 6, ?g gross, ?g net
 
 With a 10.00" liner, 14/64" nozzle throat, buna-n o-rings, simulation says
 this makes a 37% H-156, 208 Ns, with about a 1.2 sec burn.