X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=blobdiff_plain;f=rockets%2Fresearch%2Ftest5.mdwn;h=d6367784f391ef12485de4e1ace91b0039a22ac3;hp=3ea00f5a009df05739bec5c23fc2c868c7a530f9;hb=2a3ed1e87edd8541859b9e7bf1e65bb3003b7ced;hpb=adeb37527e579c29bdac8a4a1dfe06b0e5d5ec30

diff --git a/rockets/research/test5.mdwn b/rockets/research/test5.mdwn
index 3ea00f5..d636778 100755
--- a/rockets/research/test5.mdwn
+++ b/rockets/research/test5.mdwn
@@ -97,4 +97,6 @@ seconds after coming up to pressure.  The regressive curve seems a bit
 exagerated in the flight accel data, which seems completely explainable by
 the nozzle throat erosion causing pressure to faill during that period.
 
-Pretty cool for our first real flight test!
+The airframe saw an average of 12 G acceleration on the way to Mach 0.6 and
+2838 feet above the laucnh site which is at 8800 feet MSL.  Perfect 
+recovery!  Pretty cool for our first real flight test!