Path: utzoo!utgpu!jarvis.csri.toronto.edu!mailrus!tut.cis.ohio-state.edu!ucbvax!decwrl!labrea!sri-unix!larson From: larson@unix.SRI.COM (Alan Larson) Newsgroups: sci.space.shuttle Subject: Re: 104% on shuttle launch Message-ID: <30087@sri-unix.SRI.COM> Date: 30 Apr 89 09:54:38 GMT References: <883@sactoh0.UUCP> <9130003@hpwrce.HP.COM> Reply-To: larson@unix.sri.com (Alan Larson) Organization: SRI, Menlo Park, CA. Lines: 34 Jeff Boerio wrote: >My personal opinion, and something that I certainly don't know as fact, would >be that the engines used were originally expected to operate at a level X, >or 100%. But, the production engines actually operate at X+4%, or 104%. > >That's what seems a little better to me, but again, I could be absolutely >wrong. In article <9130003@hpwrce.HP.COM> howeird@hpwrce.HP.COM (Howard Stateman) write s: >You're absolutely wrong, Jeff. :-) > >Seriously, when I read your response I thought you were joking, till I >saw this last line. > >Every engine I have ever seen has had the ability to be pushed beyond its >limits. It's why they have a red line on the tachometer in your average >sports car (Camaro, Firebird, etc). I find it hard to believe that the >folks at NASA have build an engine which only operates at peak efficiency. >mostly because there is no such thing. Howard, Jeff is right. By the way, peak efficiency is not normally the 100% power point on an engine. Peak power and peak efficiency are different. Alan