Return-Path: Received: from front3.chartermi.net ([24.213.60.109] verified) by logan.com (CommuniGate Pro SMTP 4.2b5) with ESMTP id 148208 for flyrotary@lancaironline.net; Thu, 10 Jun 2004 23:51:33 -0400 X-Virus-Scanned: by cgpav Received: from [24.231.184.247] (HELO eric) by front3.chartermi.net (CommuniGate Pro SMTP 4.0.6) with SMTP id 676763746 for flyrotary@lancaironline.net; Thu, 10 Jun 2004 23:51:03 -0400 Message-ID: <00b901c44f67$50ae1bf0$0202a8c0@eric> From: "Eric Ruttan" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Pop off Date: Thu, 10 Jun 2004 23:51:02 -0400 X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1409 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1409 tinyurl.com is great for long URL's So they dont wrap. Free and easy Here is a link to RAM's ADIABATIC relief valve http://tinyurl.com/23e53 This is just like the system Mr. Kaye described. $470+$200 core. Care to guess teh weight. > http://www.ramaircraft.com/Catalog/Induction/414Ainduction/414ainduction > .htm > Lots of turbo exhaust systems to consider. > Marc Wiese > Look at the T337P. Go to RAM's website. Altitude makes no difference in > this device, just absolute manifold pressure. > Have you got a web address for this? A Google search yielded no results. > S. Todd Bartrim > Turbo 13B RV-9Endurance > C-FSTB > http://www3.telus.net/haywire/RV-9/C-FSTB.htm