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- Path: sparky!uunet!zaphod.mps.ohio-state.edu!menudo.uh.edu!judy.uh.edu!st17a
- From: wingo%cspara.decnet@Fedex.Msfc.Nasa.Gov
- Newsgroups: sci.space
- Subject: Re: Stupid Shut Cost arguements (was Re: Terminal Velocity
- Date: 30 Dec 1992 20:05 CST
- Organization: University of Houston
- Lines: 138
- Sender: st17a@judy.uh.edu (University Space Society)
- Distribution: world
- Message-ID: <30DEC199220055213@judy.uh.edu>
- References: <72527@cup.portal.com> <1992Dec29.191524.2413@iti.org> <72597@cup.portal.com> <1992Dec30.205940.28699@iti.org>
- NNTP-Posting-Host: judy.uh.edu
- News-Software: VAX/VMS VNEWS 1.41
-
- In article <1992Dec30.205940.28699@iti.org>, aws@iti.org (Allen W. Sherzer) writes...
- >In article <72597@cup.portal.com> BrianT@cup.portal.com (Brian Stuart Thorn) writes:
- >
-
- >> GRO and UARS are both candidates for return to earth.
- >
- >Doing that would cost more then they are worth. It would be cheaper to
- >build new ones and launch them commercially.
- >
-
- I would dearly love to see your cost analysis on this Allen. Since the
- marginal cost for a Shuttle mission is only 37 million dollars, this is
- what it would cost for a reflight. By the way your Titan IV cannot lift
- a payload like HST due to its adverse dynamic envelope. For a reference NASA
- publishes a guide to the environments of all major vehicles. Titan is about
- 1.5 times more harsh from a dynamics standpoint than the Shuttle. Many
- Shuttle payloads are dynamically designed for the realtively benign
- environment of the Shuttle. (+/- 10 g in the thrust direction, +/- 6 g for
- the other two axes) This is worst case dynamic load. The 3 g max acceleration
- helps to keep the true values much below this on an average basis. This
- helps the designer of a large sat flying on the shuttle to build a lighter
- satellite or this can be used to build a structure (such as HST) that would
- have a hard time on Titan. Don't drag our your tired tale of the Spy sats
- either. You have no idea what actually goes into them other than their mass.
-
- >> LDEF and
- >
- >LDEF would have been better flown as a series of smaller platforms.
- >Under those conditions it would be simple to build a vehicle which
- >returns them to Earth. That way each experimenter would get custom
- >time on orbit and the taxpayers would save billions.
- >
-
- That is your opinion Allen not an engineering judgment. There was much
- value in flying the LDEF like it was. One thing is that this gave a level
- environment for all of the experiments. If they were flown seperately, and
- at different times and orbits, there would be no conclusive comparative data
- to allow the careful analysis of the properties of the materials flown.
-
-
- >> The Hubble repair could still prove too much for orbiting
- >> astronauts and thus require return to Earth for mirror replacement,
- >
- >No for two reasons: 1) it would be cheaper to build another and fly it
- >and 2) in testimony before the House the program manager said Hubble
- >wouldn't survive the return trip.
-
- For 1) see the above. For 2) from what I have heard from the HST program
- manager at Marshall, they could bring it back down. That is a contingency if
- the solar array replacement goes awry.
-
- >
- >To date there are no payloads which can be returned by Shuttle in a
- >cost effective manner.
- >
-
- Again this is your opinion that simply is not based upon the facts.
-
-
- >> All I'm saying is that Shuttle
- >> did not meet its objectives, so don't be so sure about DC.
- >
-
- I hope very much that DC meets all of its objectives. I support the DC
- program.
-
- >Same old arguement. I guess Boeing better cancel plans for the 777.
- >After all, Shuttle failed so 777 will as well.
- >
-
- No what this poster is saying Allen is that the claims that you are making
- for the DC are exactly the claims made for the Shuttle. You through all of
- your postings have made it clear that the DC can do everything the shuttle can
- and more, which is untrue.
-
-
- >> A few weeks ago I mentioned one way that we could have kept some of
- >> that market in the U.S. until NLS, DC or whatever was ready. You
- >> said that it (maintaining Shuttle launches of commercial payloads)
- >> was too costly. Maybe so (definitely so) but those subsidies would
- >> have at least kept customers in the U.S.
- >
- >And at the same time killed any chance of a sustainable independent
- >commercial effort. If your going to do that it would be cheaper to
- >simple end all space activity.
- >
-
- Fact is no one wanted the capablility. The great leap in the market for
- communications satellites did not come until the 80's. The market for
- small LEO sats did not exist until the late 80's and now. Fact is that the
- Shuttle proved the viability of the large lift capability that is now
- embodied by its competitor the Titan IV. This market did not exist and I
- submit that it would not now if the Shuttle had not been there for designers
- to design big payloads for.
-
-
- >> Why wasn't DC-X built in 1983
- >
- >You mean when the government was spending billions killing competition
- >with Shuttle subsidies? You can't be serious; who would be that stupid?
- >
-
- You left out the most important reason in your ad hominim attack. The materials
- technology to support the possibility of the DC series SSTO did not exist
- prior to 1987. It was those pesky government supported programs like the
- B2 bomber and the NASP that provided the new generation of materials that
- allows the DC to do its job. This is straight off of the MacDac and SDIO fact
- sheet Allan.
-
- >> your argument that the next generation of boosters be a commerical
- >> endeavor? What is it they say about building a better mousetrap?
- >
- >It is hard to convince investors when they see that the largest customer
- >doesn't care about cheaper costs.
- >
-
- By the way that largest customer is that same pesky government that is keeping
- all of your space dreams from coming true. The largest customer has a great
- case of CYA. That customer cares more about the safest way to get a payload to
- space, not the cheapest. That is why uncle sugar spent three quarters of a
- billion on new boosters and over a half a billion on pad modifications.
-
- By the way you never answered my qestion of whether you would be willing to
- include the 1960 dollar cost of the development of the Atlas (5 billion) and
- the cost of the development of the Titan (5 billion for Titan I) and add
- another 4 billion for II and III.
-
- Also from what I have read, inflation is about 375% of the 1967 level today.
- That precludes a 400% rise from 74 to 86.
-
- Also to jump to another subject. The 1993 farmers Almanac lists that there are
- 111 operating nuclear plants in the US generating 21.7 percent of our
- domestic electrical energy needs. There are 8 construction permits that are
- in progress.
-
- Dennis, University of Alabama in Huntsville
-
-
-