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!burl!ulysses!gamma!epsilon!zeta!sabre!petrus!bellcore!decvax!decwrl!amdcad!amd!pesnta!peora!ucf-cs!notes From: notes@ucf-cs.UUCP Newsgroups: net.aviation Subject: Re: Commercial aircraft power-to-weight Message-ID: <2197@ucf-cs.UUCP> Date: Sat, 11-Jan-86 05:07:14 EST Article-I.D.: ucf-cs.2197 Posted: Sat Jan 11 05:07:14 1986 Date-Received: Mon, 13-Jan-86 08:06:35 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.