improve text, link to Tender Descender L3

diff --git a/rockets/airframes/MehGaNuke/index.mdwn b/rockets/airframes/MehGaNuke/index.mdwn
index fdfc016c5a0a5f6a23d047b324d3bc5545f4a168..35445aec0b0d2e45ec0b080bb03a7593fb54202b 100644 (file)
--- a/rockets/airframes/MehGaNuke/index.mdwn
+++ b/rockets/airframes/MehGaNuke/index.mdwn
@@ -117,12 +117,14 @@ ARRD released at apogee, rather than just repairing the existing airframe
 tube, we're going to build a replacement.
 
 To increase stability, the main airframe tube length will be extended from
-the original 4.5 feet to approximately 8 feet.  This will increase stability,
-allowing a reduction in nose weight.  It should also make recovery system
-loading less arduous on the rail.  This means the rocket will be closer
-to the length of an upscaled Nuke Pro Maxx instead of the original Lil Nuke.
-
-For main deployment, the ARRD is being replaced with a Tender Descender L3,
+the original 4.5 feet to approximately 8 feet.  The expected increase 
+in stability should allowing a reduction in nose weight, increasing safety.  
+It should also make recovery system loading less arduous on the rail.  Of
+course, this means the rocket will be closer to the length of an upscaled 
+Nuke Pro Maxx rather than the original Lil Nuke.
+
+For main deployment, the ARRD is being replaced with a 
+[Tender Descender L3](https://tinderrocketry.com/l13-tender-descender-tether),
 which has the advantage that the release mechanism is orthogonal to the 
 axis of flight.  That seems important when the airframe is this heavy and
 apogee occurs at a non-nominal velocity, as in the first flight.