Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 21 Jan 2003 01:10:49 -0500 Message-ID: X-Original-Return-Path: Received: from [65.66.11.38] (HELO qbert.gami.com) by logan.com (CommuniGate Pro SMTP 4.0.5) with ESMTP id 1993657 for lml@lancaironline.net; Mon, 20 Jan 2003 23:54:53 -0500 Received: by QBERT with Internet Mail Service (5.5.2650.21) id ; Mon, 20 Jan 2003 23:00:46 -0600 X-Original-Message-ID: <52548863F8A5D411B530005004759A93391AEA@QBERT> From: George Braly X-Original-To: 'Lancair Mailing List' Subject: RE: [LML] Re: Centurion Diesel X-Original-Date: Mon, 20 Jan 2003 23:00:44 -0600 MIME-Version: 1.0 X-Mailer: Internet Mail Service (5.5.2650.21) Content-Type: text/plain; charset="iso-8859-1" >>If you look at what they've already done in terms of putting a 1.7L engine (135hp) into a Piper Warrior (PA28-161) and getting performance equal to or better than the stock Lycoming O-360 (160hp) then a little quick math suggests that the thrust from a 310hp diesel might be about equal to the thrust of 370hp in gasoline. Now THAT would be way cool.<< At least one experienced pilot who has actually flown the 1.7L have reported that the "thrust" was substantially "less" than what they would have expected out of a 160Hp O-360. In one case, to the point that they felt it would not be suitable for student pilot touch and goes.