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"Jeff Findley" wrote in message
... "BitBanger" wrote in message ... $50 million for a spaceship carrying 5-7 passengers into orbit and bring them back safely? What a joke. There's no way someone will be able to claim that prize for a long time. While what you say is true, what's to stop other people, companies, governments, and etc. from donating more money to the prize? I'd personally like to see the US Government donate a few hundred million dollars each year to the pot. The longer the prize is unclaimed, the bigger the pot grows. Roton, Millenium Express, etc., were looking at around $300 million five years back. I think we have come along way since then. I expect it is doable for $200 million, perhaps doable for $100 million, with an outside possibility that a really well conceived low cost development approach unpressured by time could do it for $50 million. Space-X is not the cheapest prospect out there, but how much do you think it would cost them? Or someone else using their rockets? We are not starting from scratch any more, we have the X-Prize almost behind us with a lot of institutional knowledge, infrastructure, publicity and inertia thereby gained. A lot of the beginner's mistakes are now behind us and people have a far clearer idea of what is required. X-Prize level technology can probably be incrementally developed to orbital performance, with scaling and staging, though reentry will require something more. I think the prize is big enough, and indeed should not get any bigger, otherwise it will not be low cost. Extra money would be better spent on other prizes. This prize should be enough to induce a number of competitors to have a go at developing vehicles that are commercially viable. Many were already close to having a go on their own. I am not sure when the prize will be claimed, though I expect by 2010. To be honest, I would not be surprised if it was claimed within three years of assured funding. The ability and intent is there. Pete. |
#12
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"George William Herbert" wrote in message
. .. SpaceX is selling their Falcon V (which hasn't flown yet, to be fair) for $12 million plus range fees per flight, if you order the flight this year. That leaves you $38 million for combined R&D on capsule and eventual profit, if you care to do the accounting in that manner. A question that has been bugging me, what are the advantages and disadvantages of combining such a capsule with the Falcon V upper stage? Assuming the upper stage is to be reusable anyway. Pete. |
#13
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"Pete Lynn" wrote in news:1096688357.351813
@kyle.snap.net.nz: "George William Herbert" wrote in message . .. SpaceX is selling their Falcon V (which hasn't flown yet, to be fair) for $12 million plus range fees per flight, if you order the flight this year. That leaves you $38 million for combined R&D on capsule and eventual profit, if you care to do the accounting in that manner. A question that has been bugging me, what are the advantages and disadvantages of combining such a capsule with the Falcon V upper stage? Assuming the upper stage is to be reusable anyway. Pete. I don't think the upper stage is going to be re-usable on the Falcon 5 (or on the Falcon 1 for that matter). This is the stage that is basically in orbit, it would have to go through de-orbit maneuvers to be re-used....not really worth it. Tom |
#14
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Pete Lynn wrote:
"George William Herbert" wrote: SpaceX is selling their Falcon V (which hasn't flown yet, to be fair) for $12 million plus range fees per flight, if you order the flight this year. That leaves you $38 million for combined R&D on capsule and eventual profit, if you care to do the accounting in that manner. A question that has been bugging me, what are the advantages and disadvantages of combining such a capsule with the Falcon V upper stage? Assuming the upper stage is to be reusable anyway. I confidently posit that the R&D cost for doing such a large integration will exceed the $2-3 million in hardware saved by making an integrated stage, multiplied by the number of flights likely in the next 5-8 years. Probably even worse if you include ROI on the R&D. Several people here will object. That's fine. They can chase the prize their way. In my opinion, the cost of entry of reusable stuff is one major barrier to manned orbital operations including orbital tourism, and if someone gets the startup financing, they will likely not recover the capital costs within any reasonable timeframe. The cheap way to do the early phases is expendable. When the market expands, reusables and their higher R&D costs but lower operational costs will be the better solution. But from here to there is too far to take in one jump. -george william herbert |
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"Tom Kent" wrote in message
. 30.42... I don't think the upper stage is going to be re-usable on the Falcon 5 (or on the Falcon 1 for that matter). This is the stage that is basically in orbit, it would have to go through de-orbit maneuvers to be re-used....not really worth it. Indeed, only the lower stage is reusable at this stage. I was getting ahead of myself. Pete. |
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"Pete Lynn" :
"Jeff Findley" wrote in message ... "BitBanger" wrote in message ... $50 million for a spaceship carrying 5-7 passengers into orbit and bring them back safely? What a joke. There's no way someone will be able to claim that prize for a long time. While what you say is true, what's to stop other people, companies, governments, and etc. from donating more money to the prize? I'd personally like to see the US Government donate a few hundred million dollars each year to the pot. The longer the prize is unclaimed, the bigger the pot grows. Roton, Millenium Express, etc., were looking at around $300 million five years back. I think we have come along way since then. I expect it is doable for $200 million, perhaps doable for $100 million, with an outside possibility that a really well conceived low cost development approach unpressured by time could do it for $50 million. Space-X is not the cheapest prospect out there, but how much do you think it would cost them? Or someone else using their rockets? As has been point out already, the craft designed to win the prize does not have to be the final commerial design. And looking at Armadillo's development cycles and cost I think making a winner for less than $50 million maybe possible. We are not starting from scratch any more, we have the X-Prize almost behind us with a lot of institutional knowledge, infrastructure, publicity and inertia thereby gained. A lot of the beginner's mistakes are now behind us and people have a far clearer idea of what is required. X-Prize level technology can probably be incrementally developed to orbital performance, with scaling and staging, though reentry will require something more. And year standard off the shelf parts get cheaper and cheaper - any notice how there is a lt more things available in stainless steel nowadays compare to ten years ago? Also custom one-off design of parts can be farmed out more easyierly than years ago. At one time if you were not ordering a thousand unit of something, forget about it. Now you can order 1,2,3,... items without paying the cost of a thousand unit run. I think the prize is big enough, and indeed should not get any bigger, otherwise it will not be low cost. Extra money would be better spent on other prizes. This prize should be enough to induce a number of competitors to have a go at developing vehicles that are commercially viable. Many were already close to having a go on their own. I am not sure when the prize will be claimed, though I expect by 2010. To be honest, I would not be surprised if it was claimed within three years of assured funding. The ability and intent is there. If the prize was bigger tha it is unlikely that a winner would be CATS in design. Earl Colby Pottinger -- I make public email sent to me! Hydrogen Peroxide Rockets, OpenBeos, SerialTransfer 3.0, RAMDISK, BoatBuilding, DIY TabletPC. What happened to the time? http://webhome.idirect.com/~earlcp |
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"George William Herbert" wrote in message
. .. I confidently posit that the R&D cost for doing such a large integration will exceed the $2-3 million in hardware saved by making an integrated stage, multiplied by the number of flights likely in the next 5-8 years. Probably even worse if you include ROI on the R&D. Several people here will object. That's fine. They can chase the prize their way. In my opinion, the cost of entry of reusable stuff is one major barrier to manned orbital operations including orbital tourism, and if someone gets the startup financing, they will likely not recover the capital costs within any reasonable timeframe. The cheap way to do the early phases is expendable. When the market expands, reusables and their higher R&D costs but lower operational costs will be the better solution. But from here to there is too far to take in one jump. Yes, a capsule and Falcon V upper stage integration would have to assume a rather high flight rate. A flight rate that I hope might start to become possible in 5-8 years time. But I do wonder if this is a useful evolutionary pathway, whether this would be easier than developing a completely new reusable vehicle from scratch at that time. Say, - Develop a capsule. - Develop it towards reusability. - Integrate it with an upper stage. - Develop a version to go beyond LEO. This might be a fairly natural progression. Pete. |
#18
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Earl Colby Pottinger wrote:
A) What does big have to do with safe? Safety comes from good designs not size. Remember the Titanic? Titanic was properly designed. What killed her was faulty construction and improper operation. D. -- Touch-twice life. Eat. Drink. Laugh. |
#19
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George William Herbert wrote:
Paul Allen put about twice the X-prize value into Scaled Composites' project for SpaceShip One. They are *not* making money off the project as a whole. They may well make money off followon business. Which project? The "X-Prize attempt project"? Or the Space Ship 1 project? If you mean the X-Prize attempt alone you'd be right. But considering how Richard Branson will be licensing their know-how for approximately $20 mil, it looks like the X-Prize money will end up being gravy over and above the cost of the project. |
#20
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