Thanks a lot Mark, it is exactly what I want to know, especially 
thickness and strength.
Now I can choice some things here. 
As about number of layers, I had read the manual, and that why I was asking, 
there are just a
few words about and I wasn't sure. I am very appreciate your assistance. 

BR,
Alex Birca

-----Original Message-----
From: Mark Langford [mailto:langf...@hiwaay.net]
Sent: Wednesday, May 07, 2003 4:27 PM
To: KR builders and pilots
Subject: Re: KR>Fiberglass question


Alex Birca wrote:

>>the question is, what is the thickness and tensile strength of fiberglass
which is used for lay-up process.
May I use one type (thickness or density?) of fiberglass or it should be
different one in different area?
Where I can read more detailed info about used fiberglass in KR
construction.<<

No problem, Alex. Fiberglass typically used for all  KR construction is 5.85
ounces per yard, 18 x 18 plain weave, .009" thick, with tensile strength of
250 x  250 psi.  I'm not an expert on stock KR construction, but I believe
in most places only one layer is used, except on the wings where you end up
with  two layers around and forward of the main spar, overlapping at the
leading edge for a few inches to yield 4 layers at the leading edge.  You
probably end up with more than one layer on control surfaces as well.  All
of this is specified in the KR builder's manual.  I don't know of any place
online where these details are given, but others are welcome to chime in or
correct any misinformation I've given (from memory)...

Mark Langford, Huntsville, AL
mailto:langf...@hiwaay.net
see KR2S project N56ML at http://home.hiwaay.net/~langford


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