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|    sci.space.tech    |    Technical and general issues related to    |    3,113 messages    |
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|    Message 2,482 of 3,113    |
|    Peter Fairbrother to Henry Spencer    |
|    Re: Polythene tanks?    |
|    03 Feb 05 16:05:02    |
      From: zenadsl6186@zen.co.uk              Henry Spencer wrote:              > Peter Fairbrother wrote:              >> Powered-wings-and-wheels on a runway is about the only method presently       >> approved for scheduled public passenger transportation.       >       > You are confusing what is approved for aviation (and even that includes       > a somewhat broader range of approaches than you claim) with what is       > acceptable for spaceflight. Spaceflight, even tourist spaceflight, will       > not soon reach the level of safety achieved in aviation,              I disagree, and more, I think that's the wrong attitude. Why should       spaceflight be significantly less safe than air travel? It doesn't have to       be.              Tourists want a safe holiday. "As safe as commercial aviation" is not really       enough, it should be _safer_, as you are charging a whole lot, and thus       should be attracting the rich who will have enough money to choose the       safest airlines, or even have ther own bizjets when they want to fly.              > and it won't       > necessarily get there by using the same methods either.              Perhaps not, but we have the powered-wheeled-landing technology and       infrastructure in place already, and it's all approved and ready to go.              About the only disadvantage of PWL is that wings and wheels and engines       weigh a lot, which messes up the MR of the second stage (we are only talking       about 2-stages here, I assume, as nothing else is likely to be as       economical).              Agreed, for cargo wings, wheels and engines make little sense due to the       extra weight; but for passengers that doesn't matter a lot, the life support       and safety equipment, the seats, lifejackets, washable plastic decorative       interior, bulletproof lockable cockpit door and so on weigh more than the       weight of the wings wheels and jets, and all that has to go up too.              The passengers themselves weigh comparatively little, and the extra weight       of wings, wheels and engines doesn't matter that much, as long as you are       trying to get passengers into orbit and back, and not payload, or not trying       to do both.                     The problem with private space travel is the large investment needed, and       the main difficulties there are political, not financial or technological,       and off-topic here. Safe and profitable orbital tourism will take a minimum       investment of at least 1.5 billion, and 10 billion would be better. Sounds a       lot, but it's about the same as the development cost of a major new       airliner[1]. Boeing for instance could easily raise that much, as could       several other firms or consortia.                     [1] Building a 2-stage space transport system is technologically quite       similar to developing one-and-a-half new airliners, and then building a few       of them; but it can be done quite a lot cheaper.              You are only going to build a few, so tooling life can be shorter, which       saves a little: infrastructure is less, you don't have to build and staff a       large production line, which saves more than a little; and you do not have       to compete with highly and expensively developed present airliners       (spacecraft) - you are not trying to make a better spacecraft, you are only       trying to make a working spacecraft - which saves a whole lot. Investing       that extra billion to get a few more seats in or the fuel consumption down a       little is not needed.                     --       Peter Fairbrother              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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