use thor to post photos for corporate colors, as a test

diff --git a/rockets/airframes/CorporateColors/index.mdwn b/rockets/airframes/CorporateColors/index.mdwn
index 40e7f5fe97d80c4a537087505fcac41c39e965b8..854aa4178e735c47670710bec2c831c010e84d0f 100644 (file)
--- a/rockets/airframes/CorporateColors/index.mdwn
+++ b/rockets/airframes/CorporateColors/index.mdwn
@@ -70,20 +70,21 @@ and that design file plus all content on this page are released under the [Creat
 
 ## Photos
 
 
 ## Photos
 

-I've put all the [build photos](http://gallery.gag.com/rockets/CorporateColors/Build/)
+I've put all the [build photos](https://thor.gag.com/index.php?/tags/100-corporatecolors)

 I took together in one place.
 
 ## Result and Lessons Learned
 
 The airframe flew on 8 July 2017 in Argonia, Kansas, at a Fun Fly hosted by
 I took together in one place.
 
 ## Result and Lessons Learned
 
 The airframe flew on 8 July 2017 in Argonia, Kansas, at a Fun Fly hosted by

-the Kloudbusters at their rocket pasture.  Everything performed perfectly 
-until apogee.  The maximum velocity was 1047 m/s, or right at Mach 3.1, on the
-way to an apogee of 32,635 feet above ground.   
+the Kloudbusters at their rocket pasture.  The motor was a Loki M3464 Blue,
+and everything performed perfectly until apogee.  The maximum velocity was 
+1047 m/s, or right at Mach 3.1, on the way to an apogee of 32,635 feet above 
+ground.   

 
 Unfortunately, while telemetry shows the electronics correctly fired the 
 apogee ejection charge, clearly the nose cone did not successfully 
 separate.  The resulting ballistic return impacted about 1.1 miles down range
 
 Unfortunately, while telemetry shows the electronics correctly fired the 
 apogee ejection charge, clearly the nose cone did not successfully 
 separate.  The resulting ballistic return impacted about 1.1 miles down range

-to the south-south-west.  
+to the south-south-west, at 37 9.1739 N, 97 44.8809 West.

 
 With the final telemetry frame received from about 200m altitude on the way
 down, we know impact was at about 2/3 Mach.  Not surprisingly, then, what
 
 With the final telemetry frame received from about 200m altitude on the way
 down, we know impact was at about 2/3 Mach.  Not surprisingly, then, what