Path: utzoo!utgpu!jarvis.csri.toronto.edu!mailrus!wuarchive!brutus.cs.uiuc.edu!apple!agate!ucbvax!ulysses!smb From: smb@ulysses.homer.nj.att.com (Steven M. Bellovin) Newsgroups: sci.space.shuttle Subject: Re: Shuttle roll maneuver Message-ID: <12341@ulysses.homer.nj.att.com> Date: 31 Oct 89 02:39:42 GMT References: <1596SKI@RICEVM1> Organization: AT&T Bell Laboratories, Murray Hill Lines: 11 In article <1596SKI@RICEVM1>, SKI@RICEVM1.BITNET (David Palkowski) writes: > Question that nags me though, is why not > position the shuttle and launch assembly so the maneuver can be > eliminated all togeather ? I've always wondered, too. My tentative answer is that different missions require a different orbital inclination, and hence a different amount of roll; hence, the capability is needed no matter what. Therefore, you may as well use it on every flight, and optimize the launch assembly for other criteria, i.e., ease of travel from the VAB.