text improvement

[web/gag.com] / rockets / airframes / MehGaNuke / index.mdwn

diff --git a/rockets/airframes/MehGaNuke/index.mdwn b/rockets/airframes/MehGaNuke/index.mdwn
index 44650067056088ebc5f5b4c5386244c607ef38d1..141ac57379f58b5869df944fd5f3445fdd60fae1 100644 (file)
--- a/rockets/airframes/MehGaNuke/index.mdwn
+++ b/rockets/airframes/MehGaNuke/index.mdwn
@@ -118,7 +118,7 @@ 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.  The expected increase 
-in stability should allowing a reduction in nose weight, increasing 
+in stability should allow 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 
@@ -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
-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