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I kinda like the Direct option. It might have a better chance at getting thru Congress:
http://www.directlauncher.com/
http://www.launchcomplexmodels.com/Direct/
And the key document itself is available at any of these three URLs:
http://simcosmos.planetaclix.pt/temp/Di … v1.0.4.pdf
http://www.hays.cc/direct/DIRECT_Launch … v1.0.4.pdf
http://www.directlauncher.com/doc/DIREC … v1.0.4.pdf
I still love Ares V though. Maybe a ten-meter core stumpy/Direct option with existing SRBs?
Misc:
Look at the N-1
http://www.rolfstabroth.de/
http://www.ipms-phx.org/
Space elevator--a good payload for Direct
http://www.lulu.com/content/440980
Nice model--and I'm not talking about the rockets.
http://www.cjsaviation.com/
They will get back on their feet quickly enough.
I want to see some pix of their 200 metric ton solid stages.
I'd keep ion craft for use as probes. A two stage interplanetary probe--with a nuclear thermal stage and an ion drive payload--would achieve very great speeds and get outside the solar system pretty quick.
I was kinda hoping they would go the R-56 route--keep existing hypergolics for awile--and make a 40 ton to LEO LV. That might have been cheaper than abandoning hypergolics altogether and having all new infrastructure.
It might be just because a lot of folks aren't into beekeeping anymore.
http://www.nanotech-now.com/news.cgi?story_id=08268
The link should work now.
Space elevator--a good payload for Direct
http://www.lulu.com/content/440980
I never would have guessed this to be possible.
A great find--that link is.
I can't imagine.
What the Russians are talking about:
http://www.novosti-kosmonavtiki.ru/cont … 3/30.shtml
http://www.novosti-kosmonavtiki.ru/phpB … &start=990
Buran
http://www.novosti-kosmonavtiki.ru/phpB … &start=825
http://www.buran.ru/htm/os-120.htm
http://www.novosti-kosmonavtiki.ru/
http://www.cosmoworld.ru/eng/nk-online/
http://www.roscosmos.ru/
Looks like an R-7 LV almost.
Finally the alt.spacers see the need for bigger rockets.
Chemical is good.
Some nice images:
http://www.nasa.gov/pdf/151420main_aresV_factsheet.pdf
http://www.astronautix.com/lvs/magnum.htm
other options?
http://forum.nasaspaceflight.com/forums … 5&start=76
http://forum.nasaspaceflight.com/forums … ntid=10222
http://forum.nasaspaceflight.com/forums … entid=9638
http://forum.nasaspaceflight.com/forums … ntid=10621
http://forum.nasaspaceflight.com/forums … ntid=10617
http://forum.nasaspaceflight.com/forums … ntid=10582
http://forum.nasaspaceflight.com/forums … ntid=10583 HLLV paths
http://forum.nasaspaceflight.com/forums … 5&start=61
http://forum.nasaspaceflight.com/forums … 25&start=1
http://forum.nasaspaceflight.com/forums … &start=121
http://forum.nasaspaceflight.com/forums … 37&start=1
http://forum.nasaspaceflight.com/forums … &start=106
http://forum.nasaspaceflight.com/forums … ntid=10708 Missions
http://forum.nasaspaceflight.com/forums … entid=9668
http://forum.nasaspaceflight.com/forums … entid=9778
http://forum.nasaspaceflight.com/forums … 17&start=1
http://forum.nasaspaceflight.com/forums … =5&start=1
From http://forum.nasaspaceflight.com/forums … 45&start=1
http://simcosmos.planetaclix.pt/
Space Vehicles: A History in Patents
http://www.dataviewbooks.com/sapcecover.jpg
http://www.dataviewbooks.com/space-a.jpg
http://www.dataviewbooks.com/space-b.jpg
http://www.dataviewbooks.com/space-c.jpg
Over 260 pages of spacecraft designs from US government patent documents.
http://forum.nasaspaceflight.com/forums … entid=6541
http://forum.nasaspaceflight.com/forums … 6&posts=52
But the HLLV is the Model T. Or should be.
We do not need to use the failed ISS assembly method to build moonships.
It's a question of money.. Mir was assembled in space and it did quite ok.. ...
No--it was cramped, and was to be replaced by Polyus style Mir 2 modules-- 80-90 tons each)--abandoned because they invaded a muslim country and became overextended. And they took it out on their space efforts
Sound familiar?
That's a riot.
Space elevator concepts showing up at a convention of junior birdmen--without one shred of hope of ever fielding an LV big enough to place one tether segment up in orbit.
I would laugh were it not so sad.
Pixie dust.
Private industry alone will not win space.
Most of these space conventions are made up of a lot of groups selling and nobody buying.
Alt.space incest, I call it.
You get a few venture capitalists who forget the lesson of spacelift is TVA, not MSN. Spacelift is blue-collar thrust, not white collar computing. Venture types will put money in low infrastructure internet start ups that need only a good programmer. But the paltry funds that would cause such a venture to lift off is worthless when trying to build real spacecraft.
So space start ups get small sums in fits and starts--use them for fine glossy ads--which they just pass around to each other or the rare investor, who glances at them before placing them in the circular file..13.
Remember, the mark of a 'good businessman' is his ability to (while eating that steak dinner you just bought him) look you dead in the eye and say--
"No."
And off he goes to invest his money in EXXON.
And--to be perfectly fair...wouldn't you?
Big simple rocket on a compact pad.
You just can't beat it.
We do not need to use the failed ISS assembly method to build moonships.
Russian needs to either bring back Energiya or stick to comsat launches.
Good points. NASASPACEFLIGHT has alot of professionals compared to many other sites--like the Space.com Discussion forum with its libertarian yahoos (strange seeing that Dobbs is hardly a free trader).
Here is a thought. Perhaps a two RS-68 craft like Magnum and existing SRBs?
it is an entry-level HLLV at 80 tons--but it might get under contract before an admin. change.
So the question is:
Should the space community:
I. Support the stick and hope Ares V can survive to come later, or
II. Support Magnum, make do with 80 tons--and evolve that craft with additional solid hardpoints and growth options for that--but get this Stumpy+ under contract before we get a President /Congress liable to be more hostile to VSE and kill it altogether (With the next NASA Chief a Goldin head whose biggest LV will be Delta II again.)
At least with Stumpy or Magnum--we would be getting experience putting engines under the ET--and a wide ET may allow wide biconic craft to come along--and allow CEV to remain at 5.5--or perhaps even grow...
Thems the choices.
If I had my druthers, I'd take Ares V--but if it is Magnum...or nothing?
I'd go with the latter. Somebody get Bill Eoff back.
It looks as though this J-2 will use channel wall like the larger RD-0120 from the Energiya Core block.
I wonder what Rutan will say when the mere abort tests of the Stick wind up faster than his main craft...
Oh bah humbug, the GAO has never liked any NASA project, and neither Jeffy or the SFF will be happy no matter what NASA comes up with.
Perfectly stated.
I like your HLLV HLV (hybrid) architecture. Those winged craft would replace EELVs on their won with Magnum/AresV for the rest.
Here is how I would undertake such a scheme.
Get Ares V built at all costs.
I would do as you suggest, and then expand a bit
Consider large HLLV nuclear-electric craft under a black budget that can also be used as probes
http://www.astronautix.com/craft/intaltug.htm
http://www.astronautix.com/stages/erta.htm
http://www.astronautix.com/engines/11b97.htm
These can come later and are a bone thown to the all-science folks. This will be for cargo only and reusable. Place a station in Lunar orbit with small micro-landers for quick sample returns with the station as a safehouse.
The moon base would be near any fissure, evacuated lava tube found and filled with air.
The nuclear tug can take 100 tons to Geosynch--or the moon perhaps. Ares launched the tug and the payload in two flights.
Direct missions with capsules atop Ares V.
A lot of mass can be moved very quickly--and the science mongers get JIMO out of the deal too.
Mag-launched SSTO.
Big craft with major ground infrastructure.
HLLV
Bigger, simpler craft with mimimum pad.
Advantage, Ares V