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| Science and Technology "Somewhere, something incredible is waiting to be known." - Carl Sagan. |
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#271 | |||||
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Fleet Captain
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Re: Envisioning the world of 2100
MCT's overseas competition: http://www.russianspaceweb.com/sodruzhestvo.html Shades of Glushko's RLA http://astronautix.com/lvs/rla.htm
In the other op-ed below this which lauds space privatization as a model to fix F-35, even there the writer affirms that stealthy aircraft make poor carpet bombers. Each branch of the service had to make do with F-35. In house specialty is a must. To wit:
Speaking of the MCT project, that has started a great deal of speculation: http://forum.nasaspaceflight.com/ind...2407#msg972407 Now I don't know if these figures are accurate, but they open up modularity even greater than RLA: A 4 MCT Falcon X on the other hand would enable far bigger fairings and a much larger Heavy variant. Big enough in fact it has room for error setting 50 mt down on the martian surface. I've assumed Falcon Heavy-like LEO:Mars ratios for payloads. Methane may however allow even bigger Mars payloads due to higher Isp. Falcon X Heavy-229.14 mt to LEO (56 mt to Mars likely) Falcon X Heavy with cross-feed-270 mt to LEO (56 mt+ likely) Falcon X Ultra Heavy-382 mt to LEO (93 mt to Mars likely) Falcon X Ultra Heavy with cross-feed-450 mt to LEO (93 mt+ likely) You see you wouldn't need a single-stick core with 300 mt of launch capacity. A 4-MCT Falcon X would be much more commercially viable and you could simply use modularity to scale the payloads from 67-450 mt as needed.
http://forum.nasaspaceflight.com/ind...8396#msg108396 http://forum.nasaspaceflight.com/ind...0892#msg110892 Just remember, the Marines pushed for SUSTAIN but until Falcon Heavy, they really didn't have enough payload to have something fly out and extract troops. Which is why Dream Chaser might be scaled up to go atop Falcon heavy to where it may even have self-ferry capability: http://up-ship.com/blog/?p=17152 In terms of space debris, this was actually the worst actor: http://www.spacedaily.com/reports/Re...eport_999.html Now in terms of depots, I think even the H-2 upper stage, which is to be used right away mind you, had a problem with boil-off as per Av Week. This is due to Japans higher latitude launching point. I'll have to get back to you on that.
http://launiusr.wordpress.com/2012/1...n-the-horizon/ Not Good http://www.nasawatch.com/archives/20...n-xers-lo.html http://www.usatoday.com/story/tech/c...sagan/1644383/ BTW If you wait until you get your house in order to go to space, you never will. By never I don't mean going to space, but getting your house in order. Sadly, no ICBMs, no weathersats. |
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#272 |
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Vice Admiral
Location: I'm at WKRP
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Re: Envisioning the world of 2100
__________________
Baby, you and me were never meant to be, just maybe think of me once in a while... |
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#273 | |||||||
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Rear Admiral
Location: I'm in your ___, ___ing your ___
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Re: Envisioning the world of 2100
Once again, you don't know what you're talking about.
It's also kind of funny you name-dropping Medaris at a time like this. It was Medaris who figured out that the Saturn-I was about to be cancelled in favor of a totally hypothetical Titan kitbash being shopped around by the Air Force. That particular proposal was supported by flimsy, overly-optimistic estimates and some technical boasts so laughable they could only have been propaganda. That is exactly the dynamic right now between Falcon 9 and SLS: we know for a fact that the F9 can be evolved into a heavy lift system (the Falcon Heavy) which would more than suffice for the MPCV and anything else NASA has planned in the immediate future. In house development made sense in the 60s when NASA was in a tight spot depending on outside providers to develop their launch systems. That has long since ceased to be an issue; outside providers now have the ONLY working launch systems in America, and have taken much of the initiative in future development of new systems. NASA is no longer the leading agency in spaceflight, and even the SLS -- IF it ever flies -- will be too little too late.
__________________
It appears to be powered by some form of electricity... Last edited by Crazy Eddie; October 27 2012 at 03:56 AM. |
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#274 | ||||
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Fleet Captain
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Re: Envisioning the world of 2100
http://cosmoquest.org/forum/showthre...05#post1973505 http://cosmoquest.org/forum/showthre...71#post1967871 From what I understand he does payload integration. Now payloads often have pins in them that are to be removed after launch. I saw sometime ago, a photo of a sat with a tagged pin left in it that also had some black bands around the solar panels. You have to remove those too, or you will have problems as USA-193 did, leading to its shoot-down. "TheJim" wasn't a friend to space X either: http://cosmoquest.org/forum/showthre...t=#post1972991 A real jerk, yes, but still it is good to see passion in the real-space community. I enjoy our battles here, and despite any personal animosity--it proves that people in the business do care about spaceflight, no matter what they champion.
There are new wrinkles to the old tech. NASA is a lot like the department of Energy, which I also support for its own sake in that businessmen can always be trusted to be businessmen.
http://books.google.com/books?id=eWb...0ferry&f=false Now Sustain was going to be an EELV launched vehicle, so it stands to reason that something a bit bigger could be launched via falcon that would be large enough to sport turbojets and have some kind of return capability. The Buran analog and the original Buran concept wouldn't have come back dead-stick--and they had huge payload bays sustain would not have to have. Here is where Dream Chaser needs to focus--on contacting the folks behind HOT EAGLE because they are closer to it than the X-37/X-40 folks who are only playing with automated spaceplanes that were intended to be OSP demonstrators originally
Arsenal method still makes sense both in the public and private world for the same reason. More and more people from all walks are developing vehicles--more now than since the 50s-60s. I think this is a good thing to have a lot of approaches--and I hope they all see service. Probably not--but it is a good thing for its own sake to have a lot of aerospace folks employed and staying busy from which private companies must draw. Its not all about economics--that is what I am trying to stress. Even the EELV people are innovating with dual payloads now, as per page 36 of the Oct 22, 2012 issue of AV week.. It was on page 30 of the Oct 15 issue of the same year that we learn that the second stage of H-IIA will stay with the sat-load for a 5 hr coast, ans may need a white reflective coating to minimize hydrogen evaporation, so I imagine a depot will be more challenging. For MCT, this may play a role: http://www.nasaspaceflight.com/2012/...perators-opfs/ Remember, Ares V morphed into SLS via DIRECT's tireless advocacy, and SLS and MCT may combine. Who knows? Last edited by publiusr; October 27 2012 at 07:02 PM. |
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#275 | |||
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Vice Admiral
Location: I'm at WKRP
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Re: Envisioning the world of 2100
__________________
Baby, you and me were never meant to be, just maybe think of me once in a while... |
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#276 |
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Fleet Captain
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Re: Envisioning the world of 2100
As far as wiping the floor with me? No, he was flat damn wrong: http://forum.nasaspaceflight.com/ind...3542#msg113542 http://forum.nasaspaceflight.com/ind...4238#msg114238 Oh, no, NASA and the Air Farce are at it again http://www.spacenews.com/civil/12102...t-sharing.html |
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#277 | |
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Lieutenant Junior Grade
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Re: Envisioning the world of 2100
What a fucking idiot. |
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#278 |
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Vice Admiral
Location: I'm at WKRP
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Re: Envisioning the world of 2100
__________________
Baby, you and me were never meant to be, just maybe think of me once in a while... |
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#279 | ||||||||||||
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Rear Admiral
Location: I'm in your ___, ___ing your ___
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Re: Envisioning the world of 2100
OTOH, there is now competition between SpaceX, Sierra Nevada and Blue Origins for commercial crew, as well as between SpaceX and Orbital Sciences and (indirectly) the Europeans and the Japanese for cargo services. Killing off NASA's in-house capability hardly eliminates competition, but funneling the money that would normally be spent on an overpriced/overengineered launch system into a spaceflight industry could make that competition a lot more productive for NASA.
2) As you continue to cast about trying to figure out just who it is who opposes the SLS, you now implicitly begin to blame Libertarians/Randians. Evidently, you cannot grasp the idea that many people are looking at the same facts and the same history you are and reaching entirely different conclusions, based NOT on ideology, NOT on propaganda, NOT on op eds in popsci magazines, but on honest-to-god critical thinking.
You don't know what you're talking about.
Just like the politicians who favor the SLS are bullshitting when they suggest the system will be either on time or on cost, and they're shoveling it by the heapful if they suggest it will do BOTH.
Any of which would be preferable to the SLS: they provide launch capability for any spacecraft NASA has in service (MPCVs or Dragons and Dreamchasers purchased from SpaceX and Sierre Nevada) and continued use makes those launchers evolvable into the kind of heavy lift vehicles NASA has been dabbling with for BEO missions, especially since one of those providers is ALREADY working on a design that is both cheaper and more efficient than the SLS. In short, SLS is the OPPOSITE of the arsenal method. SLS is the same kind of crony capitalism "sole-source-no-bid-cost-plus" style defense contract that gave us the F-35.
But I'm also taking the long view of this and realizing that politics, unlike economics, isn't going to colonize space. Industry is going to do that, and the sooner we put them on the front lines of this venture, the sooner we'll start to get REAL work done in space.
__________________
It appears to be powered by some form of electricity... |
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#280 | |
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Admiral
Location: Kentucky
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Re: Envisioning the world of 2100
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#281 |
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Admiral
Location: Kentucky
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Re: Envisioning the world of 2100
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#282 | ||||||
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Fleet Captain
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Re: Envisioning the world of 2100
http://www.nasaspaceflight.com/2012/...ays-pad-stays/ The payloads are being looked at: www.space.com/18249-canada-rover-nasa-deep-space-rocket.html http://www.space.com/18275-nasa-sls-...-missions.html http://www.nasa.gov/home/hqnews/2012...6_SLS_RFI.html To quote this site: www.lpi.usra.edu/meetings/marsconcepts2012/pdf/4098.pdf "Greater performance leads to higher payload margins, faster trip times, and less complex payload mechanisms. SLS’s greater payload volume means that fewer deployments and on-orbit operations are required to execute missions." Another interesting article http://launiusr.wordpress.com/2012/1...re-expendable/ A quote from the above-described link: "Any SSTO, and X-33 holds true to this pattern, would require breakthroughs in a number of technologies, particularly in propulsion and materials. And when designers begin work on the full-scale SSTO, they may find that available technologies limit payload size so severely that the new vehicle provides little or no cost savings compared to old launchers." More work on circumlunar flights. http://www.nasaspaceflight.com/2012/...s-lunar-orbit/ In terms of a return to the moon, the same company Musk will be working with in terms of the stratolauncher, whose hanger is under construction as we speak: http://www.aviationweek.com/Blogs.as...b-51937b3bad05 Looks to be expecting work on a new F-1 engine http://www.dynetics.com/news/309 Looks familiar, what with the simplified Turbopump assembly and simple exhaust duct. Hmm. Money from SLS is going to new engines that needed a rising tide of some type to float new kerolox engines. This F-1 is to have a "New Hot-Isostatic Press Bond Main combustion chamber" with a 12:1 Channel Wall nozzle. The LFB may even be used for an Atlas replacement. "The F-1 is not a plug and play for an RD-180 on Atlas V"--but a "dual engine booster combined with an upper stage can deliver over 30 tons to orbit--a single stick version of an EELV heavy." http://www.aviationweek.com/Article....p40-510024.xml More on this pages 40-41 of the Oct 29, 2012 Aviation Week. Page 10 has yet another refutation to Dale Jensen's earlier hitpiece on Space X BTW Now we understand that MCT is not supposed to be RP, but there may already be some cross over. Now, personally, I would like to see the M-1 given new life: http://en.wikipedia.org/wiki/M-1_%28rocket_engine%29 That was a previous SLS BTW--for Lunex Now MCT looks to be private yes, but the technologies allowing for wider body cores is something Musk can benefit from with SLS paving the way for him. I wonder how much truck he has with Dynetics. What with MCT/BFR, CZ-9 and this new LV being looked at: http://www.russianspaceweb.com/sodruzhestvo.html --it is obvious that the wisdom of standard LV growth is finally being accepted.
And welcome to the board bye the way. Wave and say hello... Last edited by publiusr; November 3 2012 at 09:36 PM. |
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#283 | |||
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Admiral
Location: Kentucky
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Re: Envisioning the world of 2100
![]() I liked their turn of phrase. "Remain happily at the lauch pad". Inadvertant comic genius. |
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#284 | |||
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Fleet Captain
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Re: Envisioning the world of 2100
Better for us to clean up our own home and make it sustainable for ALL the people, not just the elites. |
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#285 | |
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Fleet Captain
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Re: Envisioning the world of 2100
1) Nothing we have brought back has served to materially benefit man that justifies the 100s of billions wasted on the bringing. 2) the cost of bringing it back will always be greater than the value gained. |
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