Xref: utzoo sci.space:5978 sci.space.shuttle:825 Path: utzoo!attcan!uunet!lll-winken!lll-tis!ames!necntc!adelie!infinet!rhorn From: rhorn@infinet.UUCP (Rob Horn) Newsgroups: sci.space,sci.space.shuttle Subject: Re: advance space news from June 6 AW&ST -- Pegasus! Message-ID: <1134@infinet.UUCP> Date: 24 Jun 88 01:14:36 GMT References: <1988Jun17.053132.5314@utzoo.uucp> <3361@phri.UUCP> Reply-To: rhorn@infinet.UUCP (Rob Horn) Organization: Infinet, Inc. North Andover, MA Lines: 27 In article <3361@phri.UUCP> roy@phri.UUCP (Roy Smith) writes: >henry@utzoo.uucp (Henry Spencer) writes: >> Pegasus, a winged three-stage design that will be air-launched from a B-52. >> [...] Payload is 600lb into low polar orbit, 900 into low equatorial orbit. > >What does a typical commsat weigh, for example? Depends on the type. Geosynch tend to be heavier. 2000kg and up. One major consideration is power supply and another is fuel for station keeping. BUT, low earth orbit fit easily in this. The latest AMSAT (Up and WORKING !!!! yeah) weights 140 kg. This kind of satellite supports packet radio techniques. DARPA has funded paper studies of a ``cloud'' of these as an alternative to geosynch. > Or a typical package of >scientific instrumentation? I've gotten data from a 10kg satellite. But there is no typical. > Or (God forbid), a typical military payload >(warhead, spysat, whatever). Spysats are HUGE, partly because optics are huge and partly because they want maneuvering capability (fuel+motor) and partly for long life. But a lot of this is the result of the present difficulty in making a decision to launch on a day's notice. (Optics being the exception.) -- Rob Horn UUCP: ...harvard!adelie!infinet!rhorn ...ulowell!infinet!rhorn, ..decvax!infinet!rhorn Snail: Infinet, 40 High St., North Andover, MA