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BWhite, if company X goes to the Dept. of Transportation to get a licence for LEO travels or beyond, do you really think that they will say no?
Now granted, they are going to check out the vehicle, launch area, require test runs, etc, but in the end they pretty much have to give the licence if everything checks out, right?
Why?
International treaties say the United States government is liable for damages to third parties if a spacecraft launched from US soil crashes in their city.
Ask foreign professors who are critical of the Adminstration whether getting a visa to attend academic conferences in the US is "easy" or a "rubber stamp" - - if the President or the Pentagon did not support your private venture. no one will say "No" but getting a "Yes" will always require one more study or impact report.
Completed in triplicate originals with 17 conformed copies.
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It would be easier to acquire your own country.
If you can afford a space settlement you could also afford to buy (no! make that contribute to the campaign fund) of the ruler of some Pacific island, ideally on the equator.
Anyhow, would could a government do about stopping a private corporation building into space, NOTHING !!!!
Aside from taxing them out of existence.
They could also deny launch permits.
The idea that North Korea or Iran might develop orbital launch capability causes apoplexy (and rightfully so, IMHO) amongst the NORAD generals.
Ain't no one going to LEO without at least one major space power actively cooperating and without at least the tacit approval of the Pentagon.
Article about why rocket science is hard.
High Technology Vs. Space Travel
http://www.spacedaily.com/news/oped-04y … d-04y.html
Reading Jeff Bell's latest and http://www.washingtontimes.com/op-ed/20 … r.htm]this and Trent Lott's preference for asphalt, I once again come to the conclusion we need a better reason "why" for crewed spaceflight.
The Ford Taurus is a rather boring ordinary American car. But how much would a 2004 Taurus cost if Ford only made 100 of them?
Although I don't like Toyota cars. The created a processes where any car can be created on any assembly line. With such technology the only real economy of scale is spreading out the design cost given all capital investment is already fully utilized and paid for. For some reason the word peg board comes to my head. ???
How much does that assembly line cost? If Toyota only sold a few dozen cars, they never would have built that assembly line. That said, flexibility is good.
Micro-chip stamping plants cost billions but stamp billions of micro-processors. Dell could never sell a Celeron machine for $500 if billions of Pentium chips were not being made each year.
The extremely-extremely-simple and disposable route has already been tried... unfortunatly, it really just isn't practical to make any rocket cheap enough to sustain a high failure rate as you would inevitibly have.
When was it tried?
The Thiokol RSRM has a 99.5% success rate and costs $30 million with a very small production run. No one has ever tried to lower that cost by buying in bulk.
Oh, and I would like to mention, Russia doesn't HAVE an upper stage engine available like the RL-12 or RL-60.
What about the http://www.pratt-whitney.com/prod_space … sp]RD-0146 Pratt & Whitney offers it for sale. Its made by the Russians.
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An RLV flown a few dozen times a year won't be cheap either.
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Edit to add. The original RL-10 is 40 years old. I am no patent attorney yet I think a number of those patents might have expired.
Therefore, maybe someone else could make knock off RL-10s if P&W declined.
Well that could be one way to earn money by the seat.
It would have financial benefits, but at the expense of the unity of mission. Rather than Americans establishing an American settlement based on certain ideas they're all familiar with, suddenly we have a multi-national crew with different views and goals trying to build a settlement. It's taking a short-term monetary gain at the expense of results later.
Besides, a direct competition with other nations would be better at furthering the program anyway, imagine a race to colonize the solar system! The progress that could be made if we have to grab prime celestial real estate before the Chinese or the Russkis, it would spread humanity across this system so fast you wouldn't know what happened. One day you wake up and Bam! Titan is petitioning for statehood.
I have this sudden urge to laugh like a super-villain. :hm:
Yup.
Five years ago, this exact thought motivated the plot premise of my almost finished book. Its frightening how we think so much alike yet reach diametrically opposed political conclusions.
:;):
Since Rev. Jerry Falwell and Rev. Jesse Jackson are both American Baptist preachers, I suspect an all-American settlement will have suffiicent diversity by itself.
Like you noted demand is everything but so is price and currently that is stopping demand. Your case of the auto was a prime example sales of Taurus versus a Cadilac or even a porche.
Catch-22 :;):
But, suppose someone drives through that price barrier, bites the bullet so to speak, and plants a permanent settlement on Mars - - damn the costs- - and along the way acquires the patents and know-how to lower launch costs and recoups that initial investment from selling that know-how to the follow on people?
You sort of hit the edge of the fence with regards to Manufacturing because known sales will be there and contractual agreements to provide a fixed quantity.
In Manufacturing for mass production not only must material cost be low but the overhead of labor as well, automation is usually seen as the answer but that entails capital expenditures and that eats away at profits.
Under contracts though there is no need to reduce manufacturing cost because it is garenteed money in the hand upon delivery for the manufacturer goods. No one cares to try to eek out a little more profit since it is already fat.
Demand is everything.
Its counter intuitive, but I believe launch costs will fall only after demand increases because increased demand will justify the production of launch vehicles as a commodity and not as a high end "one-off" product line.
The Ford Taurus is a rather boring ordinary American car. But how much would a 2004 Taurus cost if Ford only made 100 of them?
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RL-10s are not the only game in town. If Pratt & Whitney declines to sell 1000 RL-10s at $100,000 each then buy 1000 Russian LH2/LOX upper stages at $100,000 each.
Otherwise I agree. Without compeition prices will not come down.
As for Thiokol, if 5 segment SRBs don't come down from $30 million, look at liquid first stages with RS-68s and those new Northrup tanks. Robotic lasers can cut and robot assemblers fabricate and "glue" composite tanks so its all in the contract bidding.
But without several hundred or a thousand flights, no mass production.
Fly cargo independent of crew.
For cargo shots modify the mass fraction to increase fuel and reduce dry weight as much as possible. That points towards extreme disposable. As flimsy as will achieve orbit.
"If it doesn't break, it's too heavy"
For crew a smaller RLV so a more robust crew compartment can be re-used a large number of time.
A flimsy crew compartment built on the principle "If it doesn't break, it's too heavy" is plainly unacceptable. Therefore build it rugged and robust and re-use it.
But don't fly bulk cargo (food, water, fuel) in your Rolls Royce spacecraft.
PS - - I have been known to slip decimal places ???
So if I made a glaring error please tell me.
MarsDog pointed me to a link leading to this quote:
[R]elatively simple RL-10 engines cost about $2.5 million each. Gas turbine helicopter engines contain approximately the same number of parts, and are of the same complexity, but are made on assembly lines at a rate of several thousand a year. Those engines sell for $80,000. "When you are building in lots of tens, you're basically hand building these engines and they are bound to be expensive."
Is this true? Is the Pratt & Whitney RL-10 engine more complex to manufacture than a gas turbine helicopter engine? If an order were placed for 1000 RL-10s how much of a cost savings might there be per engine?
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Thiokol RSRMS cost $30 million each (that is what they sell them to NASA for) based on building 6 or 8 boosters per year.
Might mass production reduce that cost significantly? Say order 500 5 segment boosters.
The current RSRM has an 85% mass fraction. 85% of the launch weight is fuel and 15% is other stuff. 192,000 pounds of "other stuff" according to numerous sources. RSRMs are built with 1970s metalworking technology. Suppose Thiokol were to incorporate composites. Moving from 85% to 87% mass fraction would add 25,600 pounds to the upper stage payload for a 4 segment SRB and add 32,000 pounds to the upper stage payload for a 5 segment SRB.
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Looking at this, =IF= demand existed to fly 500 5 segment SRBS with an upper stage made from 2 RL-10s launch costs for cargo only would fall below $1000 per pound to LEO and in best case scenarios, fall below $250 pound to LEO.
Best case (fantasy?) scenario:
5 segment SRB costs $15 million (based on a 500 unit purchase)
2 RL-10s cost $ .5 million (based on a 1000 unit purchase)
1 upper stage fuel tank costs $3 million? (based on a 1000 unit purchase)
Miscellaneous stuff including payload stabilization until collected costs another $3 or $4 million.
(Nore - Northrup inteds their new fuel tank to be re-useable as living space and the guidance systems could be collected and returned to Earth for re-use after cargo is collected)
Lets say $20 million is our fantasy launch price. Based on statements from ATK Thiokol's Mike Kahn, such a system with 87% or 88% mass fractions and lighter upper stage tanks could well throw 80,000 pounds to LEO at a net price of $250 per pound.
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Problem? No demand. 80,000 pounds x 1,000 launches equals 80 million pounds in LEO for a total cost of $20 billion dollars.
But then, $20 billion would buy all the launch services needed to build one huge BattleStar Galactica!
Or at a 20% net to Mars delivery ration (100 pounds in LEO equals 20 pounds on Mars) - - $20 billion could send 16 million pounds of supplies to jump start a permanent settlement.
If it can shave a ton or two off a Lunar TLI stage fuel tank, or a few hundred kilos off a Lunar lander, then thats extra payload for an easy modification if the tank technology reaches a high level of maturity. About half the non-payload weight of your average launch vehicle is tankage, and a big portion of upper stage rockets too.
Shaving weight off the Earth to LEO stage is all good, also.
More return to flight http://story.news.yahoo.com/news?tmpl=s … light]cost overruns
http://graphics7.nytimes.com/images/200 … .jpg]Cocoa Beach photo
Steeple blown from Church and embedded in roof.
Space Ref and/or NASA Watch have more information. A survey team will go into Kennedy Space Center Monday morning at 7:00 am Eastern time.
http://www.cartoonnetwork.com/ppgstyle/ … ]Powerpuff Girls home at Cartoon Network.
When my daughter was younger, she would watch Powerpuff Girls as much as we would allow.
Thanks, MarsDog.
RL-10 quote:
[R]elatively simple RL-10 engines cost about $2.5 million each. Gas turbine helicopter engines contain approximately the same number of parts, and are of the same complexity, but are made on assembly lines at a rate of several thousand a year. Those engines sell for $80,000. "When you are building in lots of tens, you're basically hand building these engines and they are bound to be expensive."
http://www.rocketmanblog.com/2004/06/op … ]Rocketman blog on labor costs.
How do we lower labor costs? Build in volume.
Therefore, if we want low launch costs we need high flight rates and nothing will require higher flight rates for supplies and logistics than a permanent colony.
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Elsewhere I have mentioned using 5 segment Thiokol SRBs with 2 RL-10s for an upper stage to throw uncrewed cargo to Mars (or the Moon).
Fly 2 rockets a week (100 per year) and you need 200 RL-10s and 500 Thiokol solid segments per year. With assembly line production this new rocket (fabricated from 5 segment SRBs and RL-10s) per unit production costs should fall well below $20 million each, maybe much less. (Remember the $2.5 million versus $80,000 figure quoted above.)
40,000 pounds to LEO for $20 million is $500 per pound.
Thiokol RSRMs have 192,000 pounds of structural weight (not fuel) and were built with 1970s & 1960s materials. Use high perforance plastics in appropriate locations and the 192,000 pound figure can be lowered.
Lower it by 15% and 40K pounds to LEO becomes 65K to LEO for $20 million or less.
No fancy new science. Just the cost benefits from design improvements justified by volume.
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Demand? 100 SRB+RL10 at $20 million each totals $2 billion per year but throws 4 million pounds to LEO. 6 million pounds if lighter weight SRBs can be built.
Can lunar oxygen ever be delivered for less than that?
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What would I send to a Mars colony?
Lots and lots of http://www.miraclegro.com/]Miracle-Gro. :;):
Mix with Mars mined water and grow plants with Mars CO2.
Compost the plant waste. Combine with incinerated human waste and more Miracle-Gro and start a nitrogen cycle. Add Mars water and CO2 as needed.
I'm surprised nobody's mentioned Galaxy Quest or Spaceballs yet. They're probably the funniest "sci-fi" movies ever made and Galaxy Quest really has a lot of good comentary on sci-fi in general. Spaceballs is hilarious the first time you see it, but alas, like many Mel Brooks movies, the humor ages ridiculously quickly.
Excuse me, but there is this red thingee moving towards the green thingee and I think we are the green thingee. . .
or
EEEE-UUUU, thats just not right
Unlike Spaceballs, GalaxyQuest remains funny after numerous viewings. At least IMHO
Can anyone point me towards a link that documents the approximate cost of an RL-10 rocket engine (actually the RL-10b with carbon-carbon) or the RL-60?
In my RSO (rather smug opinion) - - unless the federal government stops being the "single payer" for crewed spaceflight (manned spaceflight is so 20th century sexist) none of this discussion really matters much.
If the VSE is go as we can afford to pay we need to get the private sector to pay more so we can go faster.
Bigelow's space hotel is the only private sector application for crewed spaceflight I am aware of that has a realistic chance of becoming real.
Well, we know for fact that this has been entrenched in NASA because that has been the entire Nixonian post-Apollo space doctern, to maximize NASA employment, and reinforced by the usual buracratic self-preservation common to large agencies, defended from real competition, and backed by many powerful politicans because of the large employment & state taxes.
Versus the possibility that Boeing or LockMart might get excessively greedy... where they can be constrained on a system-level basis by legally binding contract (more or less), where there IS competition between Boeing and Lockheed (where there is conspiring with Shuttle via United Space Alliance), and EELV prices are not that outrageous things considerd, an Atlas for ~$100M that has excelent reliability versus a ~$50M Russian R-7 if you take into account how little Russians are willing to work for.
Ah, but what about the call for DoD downselect to one EELV?
Finally, the biggest question of all for Shuttle Derived, is the army of engineers at the VAB and Pad-39 competant at operating launch vehicles efficently? It is hard to look at the Shuttle program as anything else but a make-work program that maximizes cost intentionally, and this is no longer sustainable... Are the managers willing to change their ways and do away with large swathes of long-time employees? ...Boeing's Delta and Lockheed's Atlas rockets are operated for a profit after all, Shuttle is not.
Why should we believe Boeing is immune from this same disease? As you posted earlier, no one except Uncle Sam buys Delta and it appears Atlas gets sold commercially by a group that also sells Russian/Ukrainian.
Might the occasional Atlas get sold commercially as window dressing to toss Lockmart a bone?
This whole ISS STS business might be rendered moot. ???
My mother has a condo on a barrier island near Ft Lauderdale. She is not there.
Friends tell her the islands have been closed, the power shut off and all the bridges raised to keep people off (or on?) the island.
If a heavy-lifter can be assembled from parts of smaller rockets already in production, it can be economically justified (whereas Shuttle-C et al will not likely see much profit.) Boeing could do a modest upgrade (uprated engines, more SRM's. lighter fuel tanks) or they could do something drastic and match the Saturn V.
A Thiokol 5 segment RSRM with an LH2/LOX upper stage could throw 35K to 40K (pounds) to LEO far cheaper than any other potential USA booster.
4 segment RSRM cost $30 million (a well established price based on sales for the STS program)
Add a handful of RL-10s or Musk's Merlin or the RL-10 follow on and you are in LEO at $1500 per pound or less.
An awesome light-medium shuttle derived option.
Going with shuttle C & follow on SDV with a BIG cryogenic upper stage gives a wide range of options.
5 segment RSRM plus liquid upper for about $50 to $60 million;
Shuttle C - - 2 RSRM + ET + RS-68 with cargo carrier with total RS-68 depending on payload.
Various sized ETs?
Then inline SDV with 2 5 segment RSRM and a big liquid upper stage for 150 - 200 MT payloads.
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Thiokol RSRMs have a 99.5% success rate and 100% post Challenger success rate. Why start from scratch?