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#31
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From: "303pilot" brentUNDERSCOREsullivanATbmcDOTcom
Date: 10/2/2003 10:05 AM Pacific Daylight Time Message-id: ... FWIW, I'm with Stephan, if I see "crash" I assume that someone was at the controls when the integration of the aircraft components became suboptimal for future use... Open your mind and you will find the true meaning... |
#32
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No. 2 D-KFEM Thanks. That one was 100 kg lighter than No. 1. I wonder how much of the weight reduction was due to weakening the fuselage. |
#33
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At 20:12 05 October 2003, Pat Russell wrote:
Er... Perhaps I should have asked how much of the weakening of the fuselage was due to the weight reduction. The weight reduction was mainly in the wings, by using a foam which absorbed less epoxy. |
#34
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The web site says as much as 35kg per wing could be
saved with the new method. The rest (30kg) obviously comes from a lighter fuselage.At 20:54 05 October 2003, Alex Chappell wrote:The weight reduction was mainly in the wings, by usinga foam which absorbed less epoxy. |
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