I found the instructions for the LS1 at the QBA web site (I took my own advise and look in the Resource area under Plans then LS1Canard.tiff). It does not say what the weight of the cloth is. Anyone

I need to order some cloth and my plans are at the airport. What is the layup schedule and type/weight of cloth for the top side of the LS1 canard? Thank you! Doug "Hawkeye"

Doug, Use ra7715 uni which is 7 oz and ra7725 bid which is 8.8 oz. Earnest

Thanks to Vicki & Gene Knapp who were kind enough to give Sandy and me a ride home, on their way back to Alabama. I'll have to pick up the Q-200 in a couple of days. And thanks Lynn, I did enjoy

If so go to http://groups.yahoo.com/group/everything_volksplane It is for you closet cases who wish to widen, narrow or add length to your VP fuselage and or use different types of engines. also we

For the purpose of designing the engine mount I have heard four different ideas how to allign the engine to offset torque and P factor. My question is ..Which is best for least drag? 1. AFAIK my Q

Sammy, Glad to hear you made it home. I tried to find you and Sandy at the airport at 9:30 AM to see if you wanted a ride home in the Wonder Van. Great job Jeff!! Thanks for allllll that food.

Had a great time Jeff!! You did a wonderful job again! Thanks so much! Had a fun time with the Johnson brothers (Charlie and Bob) listening to lots of stories about things that involve "smoke and

Just got back from the Sullivan Fly In and want to thank Jeff and Jill for all their effort in putting this event together. The weather made some of us nervous so we had to leave early. But it takes

Kevin and Damian, Good points. I suppose that the decision not to foam the runway had something to do with all of these considerations already being known by the powers that be. Hmmm, I wonder how my

David , yes we can reverse engineer the shape and bring it into Catia then output into a cnc program to cut it from renboard. Finesse that and use it for a plug etc etc. I see that down the road a

Damain, I suppose that you also have the means to do a three-D survey of the shape... with the obvious intent that it could then be scaled and finessed into a slightly larger shape, to accommodate an

David , yes and yes. I also have a plan for using the plug to build a hi temp CF tool to enable the use of pre-preg materials. I have several hundred pounds of CF tooling cloth just sitting looking

I think the Q.A should purchase these molds. Raoul --- "Peter Harris" <peterjfharris@...> wrote: From: "Peter Harris" <peterjfharris@...> Date: Fri, 23 Sep 2005 03:15:42 +1000 To:

I think we should all get together and purchase these molds for the QA. Raoul --- "Peter Harris" <peterjfharris@...> wrote: From: "Peter Harris" <peterjfharris@...> Date: Fri, 23 Sep

Doug, Plans have changed. Will be driving to Sullivan Saturday. Hope to see you there. Micheal Doug Humble <hawkidoug@...> wrote: Welcome Micheal! Start by going to the QBA web site

What happened to the Taylor Paper Glass process of composite lamination? Did it just die when Molt Taylor died? Laminated Kraft Paper,laminated solid fiber board and 90# liner board make good core

They could Tad, and you could build a Cub out of fiberglass, but that might take away for the whole concept. No question is a stupid question unless you ask it twice. Can't remember where I heard that

Tandem wings, of several variations, have been made of tube and rag in the past. Probably the most well known example is H. Mignet's. http://www.flyingflea.org/ But if you want to go fast there

Damian, I'll take that to mean that you are acquiring the molds and plug. Do you also have the process description for the shells (materials, layup schedule, etc.)? David J. Gall