How many Gs you will see if you don't do it right depends on how bad you
botch the maneuver.  I wouldn't have any concerns about rolling a KR, but I
have some aerobatic experience.  I would not recommend rolling anything
until you get a few hours of aerobatic training first.

Brian Kraut
Engineering Alternatives, Inc.
www.engalt.com

-----Original Message-----
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net]On
Behalf Of J L
Sent: Monday, March 12, 2007 11:32 AM
To: KRnet
Subject: Re: KR> Rolling the KR


If you do it right, you should not impose more than 1g on the airframe
in a roll.

Jeff

On 3/12/07, Larry&Sallie Flesner <fles...@verizon.net> wrote:
> At 07:50 AM 3/12/2007, you wrote:
> >For my own knowledge were does the # 5600 come from.
> +++++++++++++++++++++++++++++++++++++++++++++++
>
> + / - 7G's at 800 pounds.
>
> 7 X 800 = 5600 pounds = design maximum weight the
> structure will carry.   If your KR weighs 1000 pounds, the
> structure will still only carry 5600 pounds so 5.6 G's
> will place you at the 5600 pound limit.  Since the weakest
> point seems to be where the wing attach fittings attach to
> the spar, the only way to really know what your structure
> will support would be to test to failure.  I don't see that
> in my future.  :-)
>
> Larry Flesner
>
>
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