Return-Path: Received: from [65.54.168.125] (HELO hotmail.com) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2750669 for flyrotary@lancaironline.net; Tue, 18 Nov 2003 21:09:21 -0500 Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Tue, 18 Nov 2003 17:58:17 -0800 Received: from 65.142.114.245 by bay3-dav21.bay3.hotmail.com with DAV; Wed, 19 Nov 2003 01:58:16 +0000 X-Originating-IP: [65.142.114.245] X-Originating-Email: [lors01@msn.com] Reply-To: "Tracy Crook" From: "Tracy Crook" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Renisis Date: Tue, 18 Nov 2003 21:01:18 -0500 Organization: Real World Solutions Inc. MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0057_01C3AE17.1CF4EC40" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Message-ID: X-OriginalArrivalTime: 19 Nov 2003 01:58:17.0027 (UTC) FILETIME=[99572130:01C3AE40] This is a multi-part message in MIME format. ------=_NextPart_000_0057_01C3AE17.1CF4EC40 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Question for the list. I've seen lots of numbers thrown out there as = to how much power this engine is 'supposed' to produce. I'm wondering if = anyone has some concrete numbers as to how much 'continuous' hp's one = can expect at what rpm [what is the max continuous RPM recommended?]and = at what specific fuel burn? Also can this engine be turbo'd? I = understand from the Factory [in the Rx8] its NA. Tracy's 2.85:1 unit = should work on this engine?? As well as his electronic gizmo's? How far = is this engine as far as weights [installed] from the 13B? I've got = lots more but lets start there. [Or maybe someone has a web link they = can pass on that helps w/ these questions] I apologize if some are these = [ I suspect they probably are] redundant. Thanks Jarrett Johnson As far as I know, nobody knows the ultimate limit on continuous power = from the 13B. My guess is around 200 HP while retaining a long TBO. =20 The 2.85 : 1 drive was specifically developed for the Renesis. I = just received the specs on the Renesis crank angle sensor and ignition = timing so EC2s for the Renesis will be available before you can bolt one = on your airplane. Tracy Crook ------=_NextPart_000_0057_01C3AE17.1CF4EC40 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable

 
Question for the list. I've = seen lots of=20 numbers thrown out there as to how much power this engine is = 'supposed' to=20 produce. I'm wondering if anyone has some concrete numbers as to how = much=20 'continuous' hp's one can expect at what rpm [what is the max = continuous RPM=20 recommended?]and at what specific fuel burn? Also can this engine be = turbo'd?=20 I understand from the Factory [in the Rx8] its NA.  Tracy's = 2.85:1 unit=20 should work on this engine??  As well as his electronic gizmo's? = How far=20 is this engine as far as weights [installed] from the 13B?  I've = got lots=20 more but lets start there. [Or maybe someone has a web link they can = pass on=20 that helps w/ these questions] I apologize if some are these [ I = suspect they=20 probably are] redundant.
 
Thanks
Jarrett Johnson
 
As far as I know, nobody knows the ultimate = limit on=20 continuous power from the 13B.  My guess is around 200 HP while = retaining=20 a long TBO. 
 
The 2.85 : 1 drive was specifically developed = for the=20 Renesis.   I just received the specs on the Renesis crank = angle=20 sensor and ignition timing so EC2s for the Renesis will be available = before=20 you can bolt one on your airplane.
 
Tracy = Crook
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