Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Posting-Version: version B 2.10.3 4.3bsd-beta 6/6/85; site dg_rtp.UUCP Path: utzoo!linus!decvax!mcnc!rti-sel!dg_rtp!throopw From: throopw@dg_rtp.UUCP (Wayne Throop) Newsgroups: net.space Subject: Re: Asynchronous orbital skyhooks Message-ID: <82@dg_rtp.UUCP> Date: Tue, 7-Jan-86 12:19:45 EST Article-I.D.: dg_rtp.82 Posted: Tue Jan 7 12:19:45 1986 Date-Received: Thu, 9-Jan-86 05:34:36 EST References: <8512312026.AA15784@s1-b.arpa> <70@dg_rtp.UUCP> <1274@sdcsvax.UUCP> Lines: 42 Keywords: skyhook, tether > Question: Why wouldn't an asynchronous skyhook allow a > high-flying air-breather (or detachable part thereof) to be > injected into LEO? > Answer: A familiar scenario from previous articles on asynchronous skyhooks > is a rendezvous between a 747 carrying a cargo module piggyback, and > a tether. I think the tether/skyhook in the subsonic scenario would have to be beyond current engineering practice. My intent here was to ask if it was feasible with an asynchronous currently-designable skyhook (say, of Kevlar) to boost a cargo into LEO without using a ground catapult or any non-reusable reaction thrusters. This seems to imply a hypersonic transport of some sort, since the best delta-v from the skyhook won't boost from the near-standstill of a 747 to orbit. Note also that the investment in the hypersonic transport development would be swamped by the skyhook development costs (or so I suppose). I agree that it would be less costly to use the skyhook for the entire delta-v, but this (as far as I know) just can't be done yet. I was proposing a hybrid system to "get our feet wet" with skyhook technology. So let me rephrase. Is it possible with 198x technology to get to LEO using a totally reusable booster and an asynchronous skyhook, and would this be cheaper than using disposable or partly disposable reaction boosters. In essence this question rests on three issues: Can enough delta-v be supplied by a skyhook to make a nearly-off-the-shelf (and completely reusable) transport workable? Can some plausible and nearly-off-the-shelf station-keeping mechanism for this skyhook deal with atmospheric drag, at reasonable traffic densities? Will the money needed to get the skyhook in orbit and the transport designed and built be plausibly fundable, either governmentally or privately? These questions are left as an excersize for the interested reader :-). -- Wayne Throop at Data General, RTP, NC !mcnc!rti-sel!dg_rtp!throopw