Path: utzoo!utgpu!jarvis.csri.toronto.edu!mailrus!tut.cis.ohio-state.edu!unmvax!indri!polyslo!usc!orion.cf.uci.edu!uci-ics!venera.isi.edu!raveling From: raveling@venera.isi.edu (Paul Raveling) Newsgroups: sci.space.shuttle Subject: Re: 104% on shuttle launch Message-ID: <8056@venera.isi.edu> Date: 24 Apr 89 16:22:26 GMT References: <883@sactoh0.UUCP> <9130002@hpwrce.HP.COM> Reply-To: raveling@venera.isi.edu.UUCP (Paul Raveling) Organization: Information Sciences Institute, Univ. of So. California Lines: 24 In article <9130002@hpwrce.HP.COM> howeird@hpwrce.HP.COM (Howard Stateman) writes: >>This is little bit old, but during the last shuttle launch I heard >>one of the radio messages say "...engines at 104%..." If my memory's not too foggy, the main engines were originally certified for a given power level. After enough testing they cleared them first to 104% of that level, then to 109% for limited burn periods. > >So to carry this over to your engine running at 104%, it is running >harder than at 100%, but it is past its point of peak efficientcy, and >may do something non-user-friendly, like blow everyone all to Hell. Last night I found a note in Feynman's Appendix F to the Challenger Commision's report, where he spoke briefly about blade cracking in the high pressure fuel turbopump. Info at that time suggested that running at 109% rather than 104% would reduce the blades' safe lifetime by a factor of 2. ---------------- Paul Raveling Raveling@isi.edu