Return-Path: Received: from webserv.progress.com ([192.77.186.2]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Mon, 17 May 1999 15:37:56 -0400 Received: from progress.COM (progress [192.233.92.10]) by webserv.progress.com (8.8.8/PSC-3.0) with ESMTP id PAA06551; Mon, 17 May 1999 15:37:14 -0400 (EDT) Received: from pscserv.bedford.progress.COM (pscserv [172.16.3.250]) by progress.COM (8.7.2/PSC-1.0) with SMTP id PAA24705; Mon, 17 May 1999 15:37:15 -0400 (EDT) Received: from progress.com ([172.16.106.170]) by pscserv.bedford.progress.COM (4.1/psc2.1) id AA13170; Mon, 17 May 99 15:36:48 EDT Message-Id: <37406F42.6F1F2D44@progress.com> Date: Mon, 17 May 1999 15:34:26 -0400 From: Marcelo Pacheco To: Pine Pienaar Cc: lancair.list@olsusa.com Subject: Re: Lancair Deltahawk ??? References: <001201bea05d$0be1c260$2af925c4@default> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Pine, hope you don't mind sharing your original e-mail with the list. Official information from deltahawk is at www.deltahawk.com. The engine is probably going to be available only by the end of the year. A new engine mount will be required. The standard engine will also require a new/modified engine cowling. A inverted model is planned that will fit on a IO-360 cowling. I'm 100% commited to waiting for the engine to be available due to: 200 HP (turbocharged) at a installed weight under a 160HP IO-320. Very fuel efficient, based on published figures, should have over 6 hours of flight endurance at 65% power with the overhead tanks. 100% power up to 9000-10000 ft. 85% power up to 15000ft. Should be able to climb to 17500ft in about 10 minutes. A simple engine mechanism, no spark plugs, no magnetos. Diesel priciple combustion. Jet-A or Diesel fuel. More smooth power supply, as this engine provides positive torque throught each crankshaft revolution, while a Lycoming has 30 degrees negative torque at some point at each revolution (web site has some more details about that). That means lower stress on the prop and lower prop vibration. Projected costs a lot lower than a 200 HP IO-360. Only 4 qts of oil, no spark plugs to replace, and the engine itself is expected to cost $16K-18K. We probably don't need more than 60% power (equivalent of 75% of 160HP) for cruise, that should be available well into the flight levels, that should allow a very fast high altitude cruise. FL250 at indicated 200KTs is about 270KTAS. 5 hours at 270KTAS = 1350nm range = 1500sm. 2 stroke, V-4 design. With a constant speed prop, only 2 levers required: power and rpm. No mixture or carb heat. I'm no engine expert, and would apreciate any arguments against, short of the risk of a completely new design. I'm also intending to wait to hear back from the early users before actually putting money down. I have no association with deltahawk, but I like the ideas so much I thought our coleagues should know about it. There's a 400HP V8 design planned as well. Marcelo Pacheco Pieter Pienaar wrote: > > Hi > > I'm building a 360 and would like to find more info on the hawk engine as it > fits, and cost for the 360. > > Please help. > > Pine > pine@cpro.co.za >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html