Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!mnetor!seismo!lll-crg!rutgers!caip!clyde!bellcore!petrus!karn From: karn@petrus.UUCP (Phil R. Karn) Newsgroups: sci.space Subject: Re: Space Telescope Message-ID: <357@petrus.UUCP> Date: Fri, 17-Oct-86 02:13:26 EDT Article-I.D.: petrus.357 Posted: Fri Oct 17 02:13:26 1986 Date-Received: Fri, 17-Oct-86 22:16:09 EDT References: <1322@rayssdb.UUCP> <1250002@hpfcms.HP.COM> <180@ka9q.bellcore.com> <15@cartan.Berkeley.EDU> <8220@sun.uucp> Organization: Bell Communications Research, Inc Lines: 30 > ... And since most of the instrumentation was designed by > researchers from various universities, the space telescope is definitely > NOT a version of any kind of spysat. I'm sorry, people seemed to take my quote too literally. By "unclassified version of a spysat", I understood the original author to mean that the two spacecraft were of roughly the same physical size, mass, pointing capability and resolution, not that a surplus KH-11 was actually converted into the ST. (I'm still trying to dig up the source of this quote; I'm quite sure that I didn't invent it.) The ST and the KH-11 are OBVIOUSLY designed for entirely different missions. The KH-11 operates in an elliptical orbit and probably has orbit-changing rockets designed to optimize low-altitude coverage of interesting ground sites; the ST will operate in a circular orbit and doesn't need an orbit-changing capability. The ST is designed to optimize both image resolution and light-gathering power; obviously the KH-11 doesn't need much of the latter. Still, if the instrumentation could withstand it (e.g., through use of a neutral density filter) the ST would probably make very nice high-resolution pictures of the earth. Since it's resolution and not light-gathering power that the spooks are after, I wonder if they've tried optical aperture synthesis yet. If they could figure out a way to coherently combine the photons from two or more widely separated sets of optics (separated by, say, more than the diameter of a Titan III payload fairing or the Shuttle cargo bay which would be the ultimate limit on the diameter of a single-piece objective) then this might result in much better ground resolution than we've given them credit for. Phil