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What is the purpose of reinventing an earth to LEO vehicle besides
providing juicy low risk contracts for the US aerospace industry when a perfectly usable Soyuz is available off the shelf? Yes there is a law that NASA has successfully used to support its not invented here strategy, but the cost and time of Spiral 1 is an enormously high price to pay for reinventing yet another wheel. Wheels are useless in space. Licensing or just buying Soyuz capability to ferry people to the ISS for rendezvous with a real CEV optimized for space exploration would move the schedule forward by several years and bring some excitement back down to Earth. This would enable even more cost savings than proposed by the Independent study for The Planetary Society which recommends retiring the shuttle as soon as possible and speeding up CEV development. Using this strategy a space based CEV could be operational by 2010. Study is readable he http://planetary.org/aimformars/study-summary.html The sooner we have real people making real voyages beyond LEO the better! "How inappropriate that this planet be called Earth, when it should clearly be called Ocean." -- Arthur C. Clarke |
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![]() John Halpenny wrote: "Jorge R. Frank" wrote: wrote in oups.com: What is the purpose of reinventing an earth to LEO vehicle besides providing juicy low risk contracts for the US aerospace industry when a perfectly usable Soyuz is available off the shelf? To reduce the technical and schedule risk for Spiral 2, by giving US design teams more experience. Spiral 1 is not intended to result in an "operational" vehicle. Yes there is a law that NASA has successfully used to support its not invented here strategy, but the cost and time of Spiral 1 is an enormously high price to pay for reinventing yet another wheel. Wheels are useless in space. The law will likely remain in place because US lawmakers see Iran nonproliferation as being far more important than space exploration. If Lockheed gets the contract, they will buy Soyuz under a "technology transfer" agreement, jack up the price and sell it as american. They will launch it with their "american" Russian-engined Atlas booster. John Halpenny John, you and zzed60 are smoking crack. I can't think of a worse idea to help space exploration then to use a program held hostage by a Russian state-run agency. Yeah, that'll really help cost and reliability. There's a reason Russian space vehicles are cheaper than US, and it's not just the Russian cost of living. Soyuz is a very old design with only two-system redundancy. That means a higher probability of failure. Given, its longer flight history and better design margins have given it better history than shuttle--but that's more of a comment on how bad shuttle really is. An American designed and built capsule will be more reliable, more expandable, and better suited to future use beyond spiral 1, while Soyuz will be stuck in LEO forever. There's no point in taking a shortcut to get to Spiral 1 if that then makes further spirals untenable. That's cutting off the future for a miniscule gain in the present. Tom |
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John Halpenny wrote in
: If Lockheed gets the contract, they will buy Soyuz under a "technology transfer" agreement, jack up the price and sell it as american. If they put that in their bid, they lose the contract. If they don't disclose that until after they win, they go to jail. They won't take that chance. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
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"Tom Cuddihy" wrote in
oups.com: Soyuz is a very old design with only two-system redundancy. That means a higher probability of failure. Given, its longer flight history and better design margins have given it better history than shuttle--but that's more of a comment on how bad shuttle really is. Soyuz and the space shuttle have equivalent failure histories. Soyuz has two fatal accidents in 91 flights (#92 is in space right now) while the shuttle has two in 113. Soyuz has four fatalities in 216 person-trips while the shuttle has fourteen in 672. Do the math; they all come out to around one in fifty, or roughly 98% reliability. Statistically, they *are* equal due to the broad error margins dictated by the small population size (rough rule of thumb: if a single accident on either vehicle is enough to change the ranking, they're equal). For the same reason, none of the previous manned spacecraft (Vostok, Voskhod, Mercury, Gemini, Apollo) can be said to have greater than 98% reliability; none of them flew enough times to have demonstrated it. The fact that Soyuz has flown since 1971 without a fatality is a red herring due to Soyuz's low flight rate. Soyuz has had only 81 safe landings in the 34 years since the Soyuz 11 accident, while the shuttle had 87 in the 17 years between the Challenger and Columbia accidents. An American designed and built capsule will be more reliable, That does not *necessarily* follow. If aviation history teaches us anything, it is that reliability is maximized by 1) maximizing flight rate (i.e. gain flight experience as rapidly as you can), and 2) minimizing the cycle time between each generation of vehicles (to feed back operational lessons learned back into design). The CEV spirals have *some* chance of succeeding at 2), but not at 1); CEV will likely fly too infrequently to allow for much operational experience to feed into the next spiral. more expandable, and better suited to future use beyond spiral 1, while Soyuz will be stuck in LEO forever. Soyuz was originally designed for the USSR's failed N1 lunar program. Of course, it has been repeatedly modified since then to optimize it as a LEO space station ferry, and the Russians lack the money (and probably the institutional memory) to modify it back. So your statement is probably true, but probably not in the way you intended. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
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![]() "Jorge R. Frank" wrote in message ... To reduce the technical and schedule risk for Spiral 2, by giving US design teams more experience. Spiral 1 is not intended to result in an "operational" vehicle. Wellll, yeah, Spiral 1 is an operational ETO transport. It's just not the end of CEV evolution. -Kim- |
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"Kim Keller" wrote in
: "Jorge R. Frank" wrote in message ... To reduce the technical and schedule risk for Spiral 2, by giving US design teams more experience. Spiral 1 is not intended to result in an "operational" vehicle. Wellll, yeah, Spiral 1 is an operational ETO transport. Some people still believe that it will be, at least. The tea leaves I'm reading say otherwise. It's just not the end of CEV evolution. That's it's real purpose. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
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Jorge R. Frank wrote:
"Kim Keller" wrote: "Jorge R. Frank" wrote: To reduce the technical and schedule risk for Spiral 2, by giving US design teams more experience. Spiral 1 is not intended to result in an "operational" vehicle. Wellll, yeah, Spiral 1 is an operational ETO transport. Some people still believe that it will be, at least. The tea leaves I'm reading say otherwise. The specification is reasonably clear. It has to be an operational Earth to Orbit transport. Whether it is intended to be *used* for operational Earth to Orbit transport of people to say Space Station, is an open question. I suspect that the ISS resupply / crew transport people and Exporation Systems aren't seeing eye to eye on this. Or, at least, haven't succeeded in requiring that CEV S-1 be The Station Transport. This is actually sort of annoying on one level, but it leaves the map open for commercial transports as well. -george william herbert |
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