text improvement

diff --git a/rockets/airframes/MehGaNuke/index.mdwn b/rockets/airframes/MehGaNuke/index.mdwn
index 84131923537f9b5906fcce5a1bcf84e61b9e8020..141ac57379f58b5869df944fd5f3445fdd60fae1 100644 (file)
--- a/rockets/airframes/MehGaNuke/index.mdwn
+++ b/rockets/airframes/MehGaNuke/index.mdwn
@@ -136,8 +136,7 @@ on the main deployment bag.  For this rebuild, 3 ribs will run the airframe
 length between the 12" airframe and a concentric full-length 8" deployment
 bay, with centering rings on each end.  One sector of the rings will be
 vented to allow apogee ejection gasses to flow from the charge cups on the
 length between the 12" airframe and a concentric full-length 8" deployment
 bay, with centering rings on each end.  One sector of the rings will be
 vented to allow apogee ejection gasses to flow from the charge cups on the

-leading edge of the fin can to push the nose off without push up on the 
-main in its deployment bag.
+leading edge of the fin can to the nose, bypassing the main chute bay.

 
 ## Design / Simulation File
 
 
 ## Design / Simulation File