X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=blobdiff_plain;f=rockets%2Fresearch%2F2019-test-6.mdwn;h=831e89ae5c8cec4208f6b01b8489b4cc6ca077b8;hp=a27072f244b391c3b407920064217f656f28334d;hb=cb96cd832c0703ae747bad36079d96d7c4f147ab;hpb=0305d055eca565c3cbfa72a19f812687492fd033

diff --git a/rockets/research/2019-test-6.mdwn b/rockets/research/2019-test-6.mdwn
index a27072f..831e89a 100755
--- a/rockets/research/2019-test-6.mdwn
+++ b/rockets/research/2019-test-6.mdwn
@@ -17,7 +17,10 @@ closure were lightly greased, and the liner exterior was heavily greased.
 
 ## Results ##
 
-Test stand data in 2019-05-25-serial-3634-flight-0030-5.eeprom.
+Test stand data in 2019-05-26-serial-3634-flight-0030-5.eeprom.
+
+About a 2.5 second burn.  Sadly, we only got pressure and not load cell data,
+so no real characterization.
 
 No liner burn-through, no discernable throat erosion, nozzle end o-rings
 were fairly cooked but no evidence of blow-by.