From: Bdale Garbee <bdale@gag.com>
Date: Tue, 23 Feb 2021 04:27:43 +0000 (-0700)
Subject: text improvement
X-Git-Url: https://git.gag.com/?p=web%2Fgag.com;a=commitdiff_plain;h=018789543ab400d8b7f677c8606474235b4084d1

text improvement
---

diff --git a/rockets/airframes/MehGaNuke/index.mdwn b/rockets/airframes/MehGaNuke/index.mdwn
index 8413192..141ac57 100644
--- 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
-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