Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.1 6/24/83; site ucf-cs.UUCP Path: utzoo!watmath!clyde!cbosgd!ihnp4!mhuxn!mhuxr!mhuxt!houxm!hjuxa!petsd!peora!ucf-cs!notes From: notes@ucf-cs.UUCP Newsgroups: net.aviation Subject: Re: Commercial aircraft power-to-weight Message-ID: <2196@ucf-cs.UUCP> Date: Fri, 10-Jan-86 05:08:21 EST Article-I.D.: ucf-cs.2196 Posted: Fri Jan 10 05:08:21 1986 Date-Received: Sat, 11-Jan-86 02:55:15 EST Sender: notes@ucf-cs.UUCP Organization: Univ. of Central Florida, Orlando Lines: 5 Nf-ID: #R:trsvax:-1625033804:ucf-cs:47700010:000:182 Nf-From: ucf-cs!wahid Jan 8 16:17:00 1986 The concorde has a power to weight ratio of .5. Actually it is a thrust to weight ratio, its weight is close to that of a DC-8 or a boeing 707 by has twice their thrust per engine.