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
 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.
 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.