Return-Path: Sender: (Marvin Kaye) To: lml Date: Sat, 03 Aug 2002 23:43:24 -0400 Message-ID: X-Original-Return-Path: Received: from imo-d04.mx.aol.com ([205.188.157.36] verified) by logan.com (CommuniGate Pro SMTP 4.0b6) with ESMTP id 1681273 for lml@lancaironline.net; Sat, 03 Aug 2002 02:32:28 -0400 Received: from StarAerospace@aol.com by imo-d04.mx.aol.com (mail_out_v33.5.) id q.c9.2615bcb9 (4410) for ; Sat, 3 Aug 2002 02:32:15 -0400 (EDT) From: StarAerospace@aol.com X-Original-Message-ID: X-Original-Date: Sat, 3 Aug 2002 02:32:15 EDT Subject: Re: [LML] turbine power. X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailer: AOL 5.0 for Windows sub 124 << -ATP web site (http://atpcoinc.com) shows 16.6 GPH at 240 HP but they dont describe the test conditions. >> This would be an SFC of .46 lb./HP/hr. For reference, .7 to 1.2 are more typical numbers for small single stage, single shaft, all centrifugal engines and APU's. There are a number of well established APU and small turbine manufacturers who would sell their souls for an SFC of .46!