X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 11 Apr 2008 22:44:30 -0400 Message-ID: X-Original-Return-Path: Received: from had.dldinternet.com ([72.232.52.34] verified) by logan.com (CommuniGate Pro SMTP 5.2.1) with ESMTPS id 2842575 for lml@lancaironline.net; Fri, 11 Apr 2008 01:36:50 -0400 Received-SPF: none receiver=logan.com; client-ip=72.232.52.34; envelope-from=n103md@yahoo.com Received: from had.dldinternet.com (localhost.localdomain [127.0.0.1]) by had.dldinternet.com (Postfix) with ESMTP id 49041D90172 for ; Fri, 11 Apr 2008 00:36:13 -0500 (CDT) Received: from 12.146.139.19 (SquirrelMail authenticated user web29_bmackey) by had.dldinternet.com with HTTP; Thu, 10 Apr 2008 22:36:13 -0700 (PDT) X-Original-Message-ID: <13159.12.146.139.19.1207892173.squirrel@had.dldinternet.com> X-Original-Date: Thu, 10 Apr 2008 22:36:13 -0700 (PDT) Subject: carbon-carbon composites From: "bob mackey" X-Original-To: lml@lancaironline.net User-Agent: SquirrelMail/1.5.1 MIME-Version: 1.0 Content-Type: text/plain;charset=iso-8859-1 Content-Transfer-Encoding: 8bit > I think I missed something. > What is carbon/carbon and what are the temp characteristics? Craig: I'm glad you asked. Most of the previous replies on this subject have been misinformed. Carbon (graphite fiber) retains its strength and stiffness well up to about 2000 C. Yes... that's about 3600 degrees Fahrenheit. It does start to oxidize at about 600 C (~1100 F) in air though, so it is difficult to test to its full temperature range. Some have mentioned that "carbon composites" lose strength at 120 F or some other low temperatures. Actually, the EPOXY softens at temperatures varying with the type of epoxy. There is a wide range, but typical values of Tg (glass transition temperature) http://www.siliconfareast.com/tg.htm are around 135 C. There are higher temperature resins like phenolic or bis-maleimide with Tg of 200 C or more. One of these days I'll rebuild my engine baffles with carbon-bismaleimide composite instead of repairing the cracked aluminum. The highest temperature "resin" in common use is carbon itself. Hence "carbon-carbon composite". That's carbon fibers with carbon resin, forming a composite matrix. http://www.composites-by-design.com/carbon-carbon.htm The carbon resin can be pitch that is infiltrated into the carbon fiber preform then fired to drive off the hydrogen. The pitch shrinks leaving voids, so the process is repeated a few times. Other methods use gas-phase carbon sources to carry the carbon into the matrix. Because of the shrinkage, a final machining operation is often used to make the net shape part. The end result is lighter and stronger than steel, and suitable for use at extreme temperatures except for oxidizing flames. Space shuttle re-entry tiles and many rocket engine nozzles are made of C-C. http://science.ksc.nasa.gov/shuttle/technology/sts-newsref/sts_sys.html If you want it to look metallic AND be made of lightweight carbon-carbon, you could nickel-plate the carbon-carbon exhaust tunnels. :-) -bob mackey