Xref: utzoo sci.aeronautics:97 sci.space:14417 sci.space.shuttle:3722 Path: utzoo!utgpu!jarvis.csri.toronto.edu!mailrus!cornell!uw-beaver!sumax!quick!srg From: srg@quick.COM (Spencer Garrett) Newsgroups: sci.aeronautics,sci.space,sci.space.shuttle Subject: Re: X-30, Space Station Strangles NASP Message-ID: <6430@quick.COM> Date: 5 Oct 89 22:23:37 GMT References: <5292@eos.UUCP> <4983@omepd.UUCP> Organization: Quicksilver Engineering, Seattle Lines: 37 In article , shafer@elxsi.dfrf.nasa.gov (Mary Shafer) writes: -> -> The shuttle comes in from the north to north east. It comes "feet -> dry" at about Mach 7 and 145K ft, it's overhead at Edwards at Mach 1 -> at about 40K ft. It does a HAC (Heading Alignment Circle) to put it -> on the runway heading (usually 17 or 22), so essentially the pattern -> is about a 270 teardrop with a longish final. I think it's a 20 deg -> glidepath, with a fairly short flair. Final is flown at 285 KEAS, -> gear deployed at 275 KEAS, touchdown at 185 KEAS. (I'm taking these -> figures from Young and Crippen's 1981 SETP paper on STS-1, so the -> speeds may not be exact for any given mission, but they're about -> right.) Um, I believe that should be *towards* N-NE. Equatorial orbits are done in the same direction as the Earth's rotation, so they come in from the W-SW. (It costs an extra 2000 mph in acceleration to go the other way.) Flights employing polar orbits could come in from either N or S, but I don't think any have yet been made in a Shuttle. (And may never - I think they need the pad at Vandenburg for polar launches, and I think that's been officially abandoned.) Of course, after that 270 teardrop I believe they do land towards the S-SW, (ie - from N-NE) so maybe that's what you were talking about. The Shuttle uses *two* glidepaths on final. They fly most of the approach on a 17 degree (as I recall) glideslope, then make an abrupt pitch up to the normal 3 degree glideslope. It looks like the two intersect right off the end of the runway (where "right off" may be a mile or two at these speeds) and they only spend a few seconds (10 or 15?) on the 3 degree slope before starting the flare. Now for the questions! Is "coming feet dry" the same as extending the landing gear? I'm pretty sure I remember seeing the gear pop out *after* the flare, and I can't imagine having to design gear (much less gear doors) that could handle Mach 7! And what's the "E" in KEAS? Surely Edwards doesn't have its own standard of measurement! :-}