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- From: dietz@cs.rochester.edu (Paul Dietz)
- Newsgroups: sci.space
- Subject: Re: SSTO vs 2 stage
- Message-ID: <1992Dec31.182358.13827@cs.rochester.edu>
- Date: 31 Dec 92 18:23:58 GMT
- Article-I.D.: cs.1992Dec31.182358.13827
- References: <ewright.725755862@convex.convex.com> <1992Dec31.015157.14864@cs.rochester.edu> <ewright.725820847@convex.convex.com>
- Distribution: sci
- Organization: University of Rochester
- Lines: 25
-
- In article <ewright.725820847@convex.convex.com> ewright@convex.com (Edward V. Wright) writes:
-
- > Oh? Well, let me try again. The main cost component for reuseable
- > launch vehicles is not fuel, or even fabrication costs, but maintenance.
- > This is even more true for space launchers than for aircraft. Bruce
- > offered a careful and thoughtful analysis that would reduce fabrication
- > and fuel costs (*if* you accept his handwaving assertion that the lower
- > stage would cost less per pound to manufacture) while enormously increasing
- > the already-greater maintenance costs.
-
-
- No, he showed that for the cost of maintaining twice the number of
- stages, you get about 5 times the payload (the same scheme with
- airliners would not give a 5x increase in payload, which shows the
- problem with the analogy).
-
- You are apparently tossing in the assumption that stacking will be
- very expensive. This assumption may very well be true, but you have
- not justified it.
-
- You have also not brought out the best argument: that TSTO has higher
- development cost. Indeed, even Bruce does not suggest that TSTO be
- pursued instead of SSTO, but be kept as a backup or as a follow-on.
-
- Paul
-