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 ucbvax.BERKELEY.EDU Path: utzoo!watmath!clyde!burl!ulysses!ucbvax!space From: dietz@SLB-DOLL.CSNET (Paul Dietz) Newsgroups: net.space Subject: Re: Re: Side comment on the disaster Message-ID: <8603021937.AA03467@s1-b.arpa> Date: Sun, 2-Mar-86 12:29:23 EST Article-I.D.: s1-b.8603021937.AA03467 Posted: Sun Mar 2 12:29:23 1986 Date-Received: Tue, 4-Mar-86 01:47:16 EST Sender: daemon@ucbvax.BERKELEY.EDU Organization: The ARPA Internet Lines: 23 [debate between E. M. Smith and Bill Sebok on reusuability and size of launchers] There are additional advantages to small launchers. Generically, building a small ANYTHING is a good way to get experience before building a large economy-sized model. Small jets were built before 747s. Small rockets were launched before the Saturns. It's generally easier to try out competing technologies at the prototype stage. The motto "plan to throw one away, you will anyway" applies to any complex system, not just to software. > Reusability is a critical issue because > it is tied so closely to cost. One of the shuttle's problems is that it's not really reusable. The ET gets thrown away ($40 million (?) right there). The SRB's require extensive refurbishment. The tiles need to be inspected. The main engines require constant maintenance and rebuilding. I'd like to see hard numbers on the number of man-years of effort needed for one shuttle flight vs. a similar number for one expendable flight (including the effort in building the shuttle, amortized, and the effort in building the expendable booster). I expect the ratio is quite small.