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> The shuttle was designed with too large of a payload and too much cross-range for the missions that NASA envisioned.
Yes, but it was also largely designed for the payload & cross-range the USAF required. For fractional orbital bombardment or recon missions, a plane with a drop tank was best. The beast could carry nearly a hundred tons to suborbital trajectories if most of that were dropped on the way and the airframe were capable of using hypersonic aerodynamic lift to stay aloft to complete the single orbit mission.
If the USAF wants an aerospace interceptor/bomber, then they should have to convince congress to fund it. They screwed up our civilian HLV needs with their strategic weapons platform requirements, and then discovered that they didn't leave enough left over to get their own payloads to orbit.
The thing has carried through on graft & momentum this long.
We need this new PLS plane as much now as in the '60s. We're only 40 years late in having a sensible way to get people to orbit.
Next we need an HLV, and either the STS or Energia stacks are a good start (just get rid of the roman candles).
Shuttle-C near-term HLV
Ares HLV
Sea Dragon HLV
Some other considerations about this
http://web.wt.net/~markgoll/rse10.htm
http://www.spacecityone.com/genastro/leocheap_ch9.htm
More on large HLV design philosophy (good concepts abandoned in favor of the STS)
http://www.abo.fi/~mlindroo/SpaceLVs/Slides/index.htm
http://astronautix.com/lvs/rombus.htm
Note that people could conceivably be sent up on one, if you used enough lift capacity for a PLS or maybe even a dumb capsule, but generally, you don't want to mix crewed launch and heavy cargo.
Hear, Hear!
Humans are poisonous virus cancerous scum, and shouldn't be allowed to export our wasteful practises into the universe.
We'd be morally better off to let the universe go its way without us, and leave the Earth alone in space & time.
Do the world a favor; commit suicide and don't have kids.
The Voluntary Human Extinction Movement
"May we live long and die out"
{disclaimer: This is sarcasm on my part! I'll be back to nuke the post which started this thread, when I have time to waste later.}
Phobos Dec. 11 02
> I wonder how you will generate the effort and
motivation to build one.
The same as any other colony effort. You won't get investors & politicians and the tabloid-following general public to fund a huge space effort so that a few people can explore and eventually a few will be able to live there.
It's never gone that way. You set up infrastructure so that people & companies can survive out there -meaning make money-and that lets things grow naturally. Eventually, enough people will get tired of living in metal cans -either on a spinning rope in space or on an unnatural planetary body without healthy levels of gravity- and get together to build a better home.
Would it be any different on Mars? Can you hear the politicians laughter at the idea of settling other planets -more accurately, their apathetic silence on anything having to do with space?
The space colony designs grew out of studies of what's possible. The shapes & design choices followed not by any aesthetic choice, but of necessity driven by the environment and available resources.
They first looked at other planets and the Moon, and the overwhelming logical choice for living & working in space was space colonies, most likely using asteroid resources.
> At least with a Mars colony you can build it
up just a little over time and you don't have to
do anything drastic like rip up whole asteroids and
build huge superstructures even though those
types of things would likely naturally come into
play later on.
The thing is that if you go down to Mars, the people will have to rotate home on a regular basis (probably undergoing drastic therapy to combat long-term exposure to low-G).
And they still won't have decent living conditions.
Take the first expedition's habs (which they lived in during the trip), and let them drift in space, spinning for partial G, loosely anchored to Phobos or Diemos (Ph&D) or your NEA of choice.
Take the ship apart, and place the cargo where you can mine the NEA and set up a first generation rudimentry space manufacturing facility.
This makes mirror, volatiles (all the kinds of ices), rolled & stamped metal structures, metal cables (really the most effective use of metal mass and strength), and concrete.
Build up the truss the habs were on during the interplanetary trip, so it's long enough and strong enough to spin the now fully shielded habs (1.6 meters of concrete for space radiation) for full Gravity.
It may take a few interplanetrary throws of equipment until they can build this much, but until then, they live in the habs spinning for partial G, or in shelters buried under a few meters of dirt on the asteroid during a solar storm.
When the habs are finished, future crews have completely healthy living conditions. None of this requires any extravagant manufacturing, and the same facility that make the habitat makes metals & ices available for shipment back to LEO for sale -the first and every mission makes money this way, while seting up a permanent living outpost.
That's why I like Ph&D, even though an NEA is more attractive in terms of the cargo which can be placed there by a given rocket -conversely, a smaller & cheaper rocket can place the same cargo at an NEA as at Mars or its moons.
Go to Ph&D, and you're building up your base/first generation colony, and an exploration staging outpost for Mars itself.
> There would have to be some economic or
other reason that would motivate the building of
these massive things. I guess you could start
small ...
You see, the thing doesn't grow in one tremendous leap up to a huge colony, it makes barely enough living conditions for the amount of people there, for the comfort level they can afford at the time. It get bigger & more comfortable as it makes more & more money.
The exploration of Mars and the growth of the first off-planet colony fuel each other.
> And issues like overpopulation relief probably
wouldn't be an incentive either.
Much the same for colonizing Mars. We won't solve overpopulation on Earth by transshipping huge amounts of people in sardine cans to space. The only historical way to lower a population's growth rate is to raise the standard of living.
Eventually, space resources and the tremendous economic drive from them will have this effect on Earth. We're not thinking just a few decades ahead, but centuries & more.
Dig around PERMANENT for info about mining asteroids and products and production techniques.
> I don't trust NASA to try to develop
anything simple and to the point.
I know your feeling very well. they excell at building cash-cows and camels (for animal metaphors...) They say an elephant is a mouse built to government stnadards. I'd say a brontosaur is the NASA version, except it has 6 heads, all of which must agree on any action, so it starves to death.
Nevertheless, look at the HL-20. They were panicked that the Shuttle fleet would be grounded after the Challenger went up, and apparently there weren't too many managers and most importantly no politicians involved in the design process, so it actually was a great ship.
> If I'm understanding you right I think what your
advocating is building something like a "taxi" that just
gets you where your going and doesn't try to be
everything to everyone. I support this idea.
> We don't need to launch people on the overpriced
and complicated Shuttle just to get them to the
space station.
This thing is above all else, safe. I think it'll be cheap, if they stick with the HL-20, because (uncharacteristically for NASA) they designed it for ease of maintenance.
Lately, I'm overcome with repugnance for the Shuttle. Overgrown camel, deliberately under-capable and overpriced flying cost-overrun.
There's nothing it does which we need. Never was. They killed many good people-carriers in favor of it, when it's manifestly not safe, and they killed many excellent heavy work boosters, too.
The USAF should be told to go fish if they want a fractional orbital bomber. Somebody should be taken out & shot for going back to flying people only on the Shuttle after the Challenger died, when they cut the HL-20.
For all we could do in space by getting out there & doing real work, they decided to concentrate on a tiny overpriced gadget, just to support the contractors factories in congress-critters' political districts, and NASA's ground suport staff. And then they call it the greatest invention and let people think it's the most advanced thing ever built.
People were so shocked when the Challenger died because of course NASA must be using the very best the US is capable of making, right?
ecrasez_l_infame, June 06 2002
asteroids: What would be the feasibility of *colonizing* asteroids? I thought I'd read that they have very little to zero gravity; they are mostly made out of sheer rock (how could anything ever grow?), and they are totally devoid of atmosphere. I can understand landing on them temporarily (if our space program ever advances that far) and mining ores and etc., from them...but as for actual colonization? I can't foresee it. As I said in my first response to this topic, at least Mars is a *planet.*
1) Gravity & atmosphere, and the unstabe nature of the asteroid's structure: Don't live on the asteroids, mine them for resources to build space colonies, which will spin for full Earth gravity. Steel, rock for concrete, chemical ices for plastics and fertilizer and water.
Another point: Where do we get the idea that .38G (Mars) will be enough for us to live & be healthy? Nowhere but hope and guesswork. (wishful thinking, maybe?).
We have no idea what living long term in low gravity will do, and it's irresponsible to portray things as if we know for certain that we can live there.
We do know for certain that we can build space colonies (of various sizes from a couple of shielded tuna cans strung on a cable/truss -a station, really- to O'Neill's "Island 3") with no new inventions.
2) Asteroids are not made of sheer rock (not all of them). Some are dirty snowballs, with an outer covering of a few meters of dark dust. These are actually expended comets. Their surfaces have outgassed and left the dark dust behind, protecting the core ices left behind. These may be anywhere from a few meters across to tens of kilometers...
Even the ones we call "stony" will have ice crystals mixed throughout. Happily, they seem to have about the right amount of ices to serve as process chemicals to work the metals & rocks remaining.
Others are nearly 90% metals. Catch one of these and a CC (snowball) and you're in business -riches beyond a Martians' dreams of avarice.
3) and primarily, the contention that Mars is a *planet*
So what? Just because every human alive or dead has lived their lives on this planet, doesn't mean that's the only way to live. Not even the best way, arguably.
See the FAQ at this site
http://www.geocities.com/CapeCanaveral/ … settle.htm
Space settlement is a unique concept for colonization beyond the Earth. While most thinking regarding the expansion of the human race outward into space has focused on the colonization of the surfaces of other planets, the space settlement concept suggests that planetary surfaces may not be the best location for extraterrestrial colonies.
Artificial, closed-ecology habitats in free orbit would seem to have many advantages over any planetary home (Earth included).
Another aspect of this, Since Mars is a planet, it has a lot of stuff in one place. This is usually taken as a good thing, since you have "everything needed for a civilization in one place".
Problem: that "one place" is a whole planet! and planets are huge! Too much gravity to let you move round easily outside your habitat (while not being enough inside your habitat), too much to let you move anywhere else in the solar system for commerce.
Mars has a nearly 24 hour day? So what. That only means that you're stuck with 12 hours of night. On Mars, you need to expensively import nuclear reactors from Earth. At an asteroid, point a metal foil mirror at the Sun, and you're set up.
Geothermal? please. The planet's core is dead. No magnetosphere means no magma. The volcanoes tell the story: a long time ago, they grew big (multiple overlapping impact craters inside the calderas). Large volcanoes means that the surface of the planet doesn't move over a liquid core.
It's a dead cold rock, with maybe a few outgassings. Hardly the making of a civilization, when asteroids are flying mountains of ice, with a fusion furnace right nearby for energy.
Mars has evidence of subsurface ices. We know for a fact that asteroids (and Mars' moons, interestingly) have ices by the gigatonne, and no prospecting. Land, scoop up some stuff, and heat it; steam comes out.
Look at some of the old NASA images of space colonies on that site I linked to.
No new inventions needed to mine asteroids for materials to build these things.
Lots has been said about how odd it would be, living inside a huge spinning can.
Live on Mars, and you're stuck inside a tiny can, and if you go outside it, you're in a suit! a pink sky! (low gravity makes our bones & muscles weak, so after your 1.5 year surface exploration stint, you go back to Earth on a stretcher to spend the next 15 years rehabilitating. Prove I'm wrong...)
Many people on Earth never leave their home town for years at a time, never explore mountains, never see the ocean or forests.
In a space colony, you have no sunset, but you've got the stars like nobody on Earth has ever seen them, and if your colony is near a planet, you've got it anytime you look out and you can go visit anywhere.
They did studies on living inside a colony like this. They specifically designed them for long sight-lines and roomy interiors.
People would work for days in old US Navy dirigible hangars. a 30 meter high ceiling, and little office cubicles inside them. People come outside their offices, and take a smoke break "outside" under the hangar roof!
The point is that people live in all osrts of places, and a space colony is just a lot more likely to be feasible and profitable than terraforming a whole bloody planet.
Mark S Oct. 17 2002
>The word from the World Space Congress says that NASA will refocus the scope of Space Launch Initiative. Instead of leading to a new RLV, it will produce a crew rescue & transfer vehicle for the ISS and upgrade the shuttle.
Mark S
Oct. 23 2002
> I think SLI had the wrong idea by trying to build a "one-size fits all" vehicle for both cargo launch and crew launch.
Phobos Oct. 25 2002
> Instead of pouring money into a new rescue vehicle for the ISS, NASA should just contract with Russia to keep a Soyuz up there. Even though we'd be paying Russia for such a service it'd probably be cheaper in the long run than having to redesign the wheel.
Alexander K. Naylor
Dec. 03 2002
> The thing that we need is a simple escape vehicle for the ISS, not some over-complex-brimming-with-new-technology Dyna-Soar revival ship. In my opinion, the best thing would be something like a six-person Voskhod.
There were referrences to a new fully reusable 2 stage vehicle, as the "replacement" vehicle, so this is a new wrinkle. The smaller spaceplane, seemingly part of the newer SLI contracts is a different animal.
Don't make the mistake of calling it a "Mini-Shuttle" as the articles do.
Unless they go overboard and make the mistakes of the CNES Hermes spaceplane, it won't be a minishuttle.
The Hermes tried to do too many things at once, and got too big & expensive and was cut. The Shuttle did the same thing, and while it didn't die, it became too big & complex to do anything well. (A camel is described as a beast designed by comittee: smelly, bad tempered, with humps. At least the real camel does some things well.)
The SLI spaceplane is described as "a crew-transfer vehicle instead of a limited-use crew escape pod for the space station... it would be more cost-efficient for NASA to develop a multipurpose ship."
This still doesn't mean a camel. Multipurpose crewed access vehicle covers launch, flight, and re-entry, with assured crew survival in all flight regimes -something the Shuttle has none of.
The Shuttle isn't particularly safe for crewed access: no escape system, since a big cargo hauler is too big for escape rockets. This is where the HL-20 type PLS really helps.
Let's just hope NASA sticks with this small vehicle, and doesn't try to tack on too many extras.
We treally do need this. The Shuttle is a death trap, and it's long past time that we found a safe way to get people up there. The Soyuz isn't old & unreliable, it's just old. It's endured because it's highly reliable. The problem is that it subjects crew to high G loading on re-entry and "thump-down", and unlike a spaceplane, and it's expendable.
Some background on PLS:
The current designs being floated for the spaceplane are strongly reminiscent of then old HL-20 PLS (Personnel Launch System) of the late '80s.
The follow-on evolved version HL-42
Scroll down to the Grumman/OS SLI concepts
http://www.slinews.com/concepts.html
2 that are particularly nice are the simplest:
One is the HL-20 on an ELV, the other is the HL-42 on a RLV
This in turn was derived from the Soviet sub-scale spaceplane rocket tests of the early '80s which were originally to be tests for their UruganSpiral space interceptors.
Note that the Spiral was a competitor to the USAF X-20 Dyna-Soar orbital interceptor/bomber.
http://deepcold.com/
So, NASA's new hope apparently draws on the earliest days of NASA manned spaceflight, and military space projects which never got off the drawing boards (though parts of the X-20 were the first pieces of hardware for manned spaceflight which actually were built).
It is also interesting to note that the insistence by NASA that the idea of a crew spaceplane going up on ELVs is completely new, is bogus. They are apparently ignoring the HL-20 and X-20 work (note the really good work & thought that went into the HL-20 It's not just a modernization of the Dyna-Soar, it's a total crew treatment).
Far from being radically new, this spaceplane goes back to spaceflight history, back to things which made sense then, and still do, things they canceled in favor of continuing to rely on the Shuttle, experimenting with SSTO in the X-33 fiasco, building the seemingly deliberately overly-complex & expensive ISS, and the station lifeboat X-38.
NASA Proposes New Space Plane, More Money for Shuttle
09 November 2002
http://www.space.com/missionlaunches/fl … 21109.html
CAPE CANAVERAL, Fla. -- NASA has decided to build a new space plane to carry astronauts to and from the International Space Station, government officials said Friday.The proposed orbital space plane, which could be launched from Cape Canaveral aboard an emerging breed of rockets, is part of a sweeping overhaul of the space agency by Administrator Sean O'Keefe.
... In addition to the new vehicle, O'Keefe's plan calls for spending more money to upgrade the current shuttles so they can keep flying through at least 2015.
In keeping with the Bush administration's spending policies, the new space plane must be developed within the confines of NASA's current budget forecast, which is about $14.8 billion a year
The orbital space plane could use launchers already being developed by The Boeing Co. and Lockheed Martin Corp., which would save money by avoiding the cost of creating an entirely new launch system, as was done for the shuttle fleet. The companies have new launch complexes on NASA and Air Force property at Cape Canaveral.
Boeing and Lockheed executives confirm they have been working with NASA to figure out what it would take to prove the rockets are safe to launch humans.
www.nytimes.com/2002/11/1...7c&ei=5062
NASA announced... it would delay development of a replacement for the space shuttle and instead start work on a new, smaller orbiting space plane ? a sort of minishuttle ? to take people to and from the ISS.Under the plan, the four ships in the 20-year-old shuttle program would continue to fly until at least 2015, and perhaps more than five years after that. This strategy delays a decision on a shuttle replacement until the end of this decade, said Sean O'Keefe, the administrator of the space agency, and gives the NASA time to define better what the new vehicle will be.
www.space.com/missionlaunches/fl_021030a.html
If a new ship piggybacks on a rocket, it might fly at the same time shuttles are flying and serve a different function, Boeing and Lockheed Martin officials suggested.Such a ship could be used to supply the space station or act as an emergency escape vehicle, replacing the Russian Soyuz ships used as escape capsules, Laffitte said. Soyuz production is guaranteed only through 2006, and Russian officials have threatened to stop production early due to lack of funds.
"I think those will be the two areas that we will get started," Laffitte said, before attempting to make the ship a replacement for the shuttle.
Still, he admitted, "man-rating" a rocket so it's considered safe enough for people could be a difficult job.
The rocket concept is just one option under study, Kennedy Space Center Director Roy Bridges said.
"That's the way we got started, so obviously we were able to do that in the earlier days, and of course we have more capable vehicles now," Bridges said.
Boeing's Trafton acknowledged the buzz about the rocket option. "There is increased interest in using expendable launch vehicles to launch a winged vehicle of some kind to space and to space station," Trafton said.
The SLI approach to designing a new ship is different from anything NASA has attempted, Dumbacher said. "In addition to the performance, I have to address cost and reliability/safety, and that's something that hasn't been done before in the rocket business."
which is troubling to hear, since it says they're being paid to do all that good work over again.
Note also, the larger HL-42 spaceplane; That reusable flyback booster would be great on its own. Note that it puts ~30 tons into LEO, and that neatly replaces the Shuttle. (Just don't let NASA hear that! It just shows that the Shuttle is way beyond useful. It's nothing but jobs, and it does nothing we need it for. Somebody should be taken out & shot for cutting the HL-20 back in the '80s, and going back to flying crew only on the Shuttle.)
It's also nice that the boosters and the spaceplane don't rely on each other's development. The plane could go up on expendables, and the boosters can do anything.
Other soviet spaceplane concepts (really, nothing the SLI has looked at is entirely new).
(MiG 105 Sub-sonic and air-drop test plane)
http://www.astronautix.com/craft/mig10511.htm
Yes! for ferry-go-around engines. For my money, lose some cargo, and put an engine on the HL-42.
http://www.astronautix.com/lvs/spil5050.htm
http://www.astronautix.com/lvs/bizan.htm
http://www.astronautix.com/lvs/system49.htm
http://www.astronautix.com/craft/maks.htm
I like thinking & reading about interstellar travel -I like mental masturbation almost as much as the real thing.
But that's all it is.
I don't care about interstellar. Get some of us off this planet, making a living, and expanding the livable area/volume available to life out off this one rockball.
Interplanetary is quite enough challenge for us, locked up down here at the bottom of a hole 8km/sec deep.
Another aspect of it, goes back the Fermi's question about ETs ("Where are they") and Dyson's belief that we, ourselves or whatever we evolve into, should be able to live on past the death of the Sun, and on to the end of the universe. We just have to expand off-planet! No new inventions needed to start.
With techniques we can think of now, and no new fundamental discoveries in theoretical or applied science, we can foresee ways to get to all the nearest stars within a thousand years. Ten-fold greater time, and we're on our way across this entire galactic arm. Another ten-fold jump in timescale, and we're across the galaxy and on the way to others.
What ever particular you want to debate about -life support, engine & power supply, biomedical, or what, if we don't know the best way, we do know several ways which will work.
Don't hold up the first steps into the solar system, becuase we don't know for sure how to go to the stars.
Anyway, all I mentioned in my earlier post, was using this particular effective technique we've got -nuclear pulse rockets- to go into the solar system. Not it nor anything else close to moving off the drawing board into a laboratory curiosity helps much with interstellar travel.
We'll certainly never leave the Solar System though until we get over our fears of radioisotopes or discover some other means of generating comparable energy and it definately won't be solar cells or liquid hydrogen.
hear, hear. You make my point.
I can't see there being any kind of political support for using nuclear explosives in space even if they're being used for peaceful purposes.
I choose not to argue for the ignorant hysterical view that anything relating to or containing the words "radioactive" or "isotope" or "nuclear" is evil.
Nuclear pulse is the best tool we've got, and I'm not going to forget about it because of their irrational fears about a certain class of technical innovation.
Read those CDI articles about a multinational effort to use discarded weapons to fuel a spaceship.
All it takes is what the Mars Society is doing. Get something hoepful going, get some notoriety, and some following. Get the general public to see what's going on, and get more & more support.
By the time you need an intitial mass in LEO of several hundred tons (like many mission proposals out there), and want a few hundred tons of cargo delivered to Phobos for the Mars base, then you start educating people on the realities on nuclear pulse:
1) There is no possible way -at all in this universe- that our use of nuclear pulse engines will hurt anything in interplanetary space. (Yeah, yeah, we could ram the ship into an asteroid, but does that really hurt anything?)
2) the Pu is there. We're glad the warheads are dismantled, but the job's not over yet. The stuff is worth more than gold or just about anything else inorganic, and the only other proposals being floated to get rid of it, involves polluting it past the point of being useful for making a bang, and burying it, where we'll have to guard it for 100,000 years until it decays so it can't be re-refined.
3) We have an incentive to get a large, robust ship & payload to Mars -quickly and cheaply.
4) the Pu and NPR is the best way to do it -and get rid of the Pu.
5) Oh, yeah. It helps foster greater international cooperation in dealing with nuclear materials and energy, and it helps foster disarmament in an atmosphere of doing something large-scale, long term hopeful for the future, and which brings us closer together as it gets us Out There.
You do the math.
Pluto's not completely without atttraction. It's surface ices should be an interesting mix of stuff from before the solar system formed.
There will certainly be continents of ices -all sorts of ices, and with low G and no atmosphere it should be a piece of cake to lift them into space to a space colony construction site nearby.
Problem is, you need lots of mirror area to collect sunlight. That's not really a problem; use power beaming to send power down to the facilities and explorers on the surface.
You should really think of some arguments and debating points to start a discussion rolling. Your comments about Mars stink. Recycled urine is pretty much what we've all been drinking all our lives, along with water dried out of corpses, and food grown in fields sown with human dead -in space, it's just a little more direct! It's also more pure, being distilled or reconstituted from H2/O2.
Also, at Mars, we can get all the H2O we want at the moons. Lots easier to get a self-sufficient base up there, and full G for the habs.
With modern high performance drives (nuclear pulse especially) the travel times to Pluto & back aren't as bad as we think, being restricted to expendable chemical rocket fireworks at present. The whole solar system is open to us, if we think ahead. (even out in the cometary halo -you just need a really big mirror!)
Lots of hysteria and mis-disinformation here.
First: Who says $200 billion? Let me guess, the program's detractors!
Second, and by far the bigger question, Exactly what are we talking about?
The term "Star Wars" was coined by detractors specifically to throw ridicule on something they didn't like.
Go ahead and let your preconceptions show, if you want, but you're only hurting your own credibility about being capable of a rational discussion of the subject.
Go back to Reagan-era SDI porposal and what were they talking about? Terminal phase and theater AA missiles on steroids. (THAAD and the Navy's cancelled SM2ER-block 4 for example.)
Nobody seriously talked about "thousands of nuclear powered armed laser space fortresses" except the detrators (Where the $200 billion and higher price estimates came from -and that only if using the flying cost-overrun Shuttle to lift everything).
Read Freeman Dyson on ABM. Entirely rational discussion sheds much light. (not the hysterical, nearly conspiracy theorist detractions we hear which are unquestioningly accepted by the mass media).
(I think this was from the book From Eros to Gaia)
If, as SDI and NMD talk about, Theater/Terminal defenses are looked at (T/T ABM), the entire menagerie of phantom bogeymen thrown up against ABM dissapears.
It does not require space assets, except for more of the standard EW satellites and redundant C3I capabilities we already have.
Don't worry about boost phase, because that's not likely: It requires space-based weapons, which do threaten your potential opponents. An orbiting weapon capable of hitting a rising ICBM could also hit the politburo members while they're on vacation at a beach on the Black Sea. It necessarily requires C3I capabilities which can reach out over the enemy territory, and the fog of war makes this highly unlikely.
You're always advantaged, and the enemy is disadvantaged if the battle is being fought over your terrain.
Hence T/T ABM. Deal with the threat after the missile busses have deployed, and the decoys are out -all the cards on the table, no deception. Hit them all, or discern the real threats, which ever works.
BTW, even fielding an ABM works, even before a single shot is fired. Decoys, you say? A missile lifts so much. Add more mass, and the missile doesn't lift as well. Add decoys, and you must lose either warheads or range. Right there, your defenses have cut the attacking force down, eh? Even before that, you force them to do R&D on their countrerss to your defenses, adding more time and causing them to build fewer missiles. Again, you've stopped an attack from getting through before a shot is fired.
T/T ABM doesn't threaten the enemy. It only applies defensive force over your terrain.
It doesn't require nuclear weapons, it doesn't require energy beam "Death Rays".
Note that the Russians were in favor of multilateral ABM in the early days of NMD.
For decades, they've fielded early generation ABM in their SA-5 SAM system. They were entirely enthusiastic about bidding on the contracts for multilateral ABM.
Doesn't sound too destabilising -quite the reverse, and I wonder why people didn't see the hyypocrisy of the detractors when they didn't seize on this: It removes some fear of the good ol' boys spending too much money among themselves, by spreading the contracts out around the globe. It fosters stability, by easing up on secrets among unsteady partners, making them more steady friends. It defends everybody against small-scale attacks, and accidental launches.
The detractors screamed all the louder. They don't care about workable answers, they only want to force their world view on everybody (the impossibility of unilateral disarmament is all they offer. "Sit around in a circle and hold hands and sing! That's the answer for peace!")
As for hurting the Chinese delicate sensibilities by fielding ABM and de-fanging their nuclear threat and the deterrance of their weapons, I don't care a bit. They can cry into their tea.
They want to threaten our cities with nuclear fire. I'm all the more happy to remove the threat. Not that I believe ABM is a "Shield"; only the detractors use that term, to make it sound more impossible. A good defense doesn't need to be 100%. Just cast enough doubt in the enemy's mind to cause him to hesitate or forestall attacking, and your defense is 100% effective.
It makes me sick to hear anti-war people talking in favor of MAD! Insane! Totally morally & intellectually bankrupt, to speak as if the "method of preserving peace for the last 50 years" is the best answer! (Until we can convince the Pentagon to turn all their weapons into prayer wheels, anyway.)
I don't consider the Chinese or N.Koreans to be much of a threat. They know full well that we wouldn't hesitate a moment to eradicate every military base, rail head, deep-water port, and large city of theirs if we detected a launch. They would cease to be a civilised power of the 21st century if they tried it, and everybody (but media outlets) knows it. A dozen or so old-fashioned liquid-fueled boosters? Don't make me laugh.
As for the Pu239 from all those decomissioned missiles, I say we make it into thousands of identical small yeild bombs. Multilateral effort to account for and dispose of tons of weapons-grade stuff, by doing a large-scale multinational space mission. Send 20 people to Mars, with the seeds of a colony among the moons and a permanent exploration outpost.
Use the same technology of a city-killer bomb to get humanity out into the stars! After we use up all the warheads, build breeder reactors to make more Pu239 for more spaceships! Build more nuclear power plants on Earth to make more Pu, to get us out there, so we can eventually remove all the heavy polluting industry from the face of the planet and get out into the solar system permanently (Nice circle of answers to a lot of our problems, huh?)
2 articles about this "plowshares" idea.
Note that the CDI is most definitely not "hawkish" on defense. You should agree with them, and they are a necessary tool for understanding the military spending. Knowledge of the Defense Monitor is the first credential I look for in anybody talking out against war.
Orion will rise! - CDI - Part I
Orion can rise! - CDI - Part II
> Yes, I'm still 100% in support of manned missions to
Mars, with the goal in mind of not only exploring it, but
settling and eventually colonizing it
I agree, with some provisions (below)
(Working with the M.S. since 8/98)
> As regards the *rest* of the solar system, however, I've
come to agree with Byron, who said at the "Europa"
discussion: "That's why I have the firm belief that Mars will
be the only place in the Solar System (besides Earth, of
course) where humans will be able to establish any kind of
meaningful society..." -and- I've come to agree with Aetius'
vision of using O'Neill settlements "out amongst the gas
giants."
I take it further, that free-space colonies (colonies in space rather than on planets or bodies) are the long-term way to go, and the short term best way to livable conditions.
Mars is usually taken (quoting Dr.Z.) as the best place because it's got everything we need in one place.
So does a space colony. By the time the infrastructure exists in space to build a colony anywhere off-earth, space colonies are the best way. You'll need as much infrastructure if not more to build on a planet, and if you've got it, then the colony isn't too far away from anywhere (travel-wise, which is the important thing in space. Getting on to & off of a planet is hard).
NEAs can be used if building in the Earth-Moon system, and Phobos/Diemos can be used at Mars. When you've built one, you've got anything & everything you need to support it or build another.
A facet of a planet's having "everything in one place" is the fact that this place has a lot of gravity. Too much to be convenient for travel. At the same time, this probably isn't enough for us to have enough gravity to live there!
In a space colony, you've got full Earth G and full radiation shielding, for complete healthy living conditions. It's almost impossible to get this on another planet.
As to going to Mars ASAP, the moons are the key. Excellent resources (2 whole mountains of water and many other chemicals near at hand on the first landing -anywhere on the moons!), and better living conditions than you'll ever get on the planetary surface (and free unlimited solar energy. Lots better than hauling out and soft-landing a nuclear power station).
Send people out there to live sooner, since there'll be no need for them to return to Earth to rehabilitate after a tour of duty in Mars' low gravity.
The first manned Mars mission gets water and starts building the spinning habs for fully Earth-like conditions. Later missions build up the seed factory planted there, to pick the base up by its bootstraps to build up to being able to make a real colony, far sooner than terraforming (if that will ever be feasible).
Make money on the first and every mission by bringing back tanks of water & chemicals.
Check the FAQ at Mike Comb's excellent space colony site
http://members.aol.com/oscarcombs/settle.htm
Look especially for the parts about the advantages of space colony living over planetary living.
As for colonies out around Pluto, again, don't go down to the planet, except for exploration and maybe resources. Live in space, with full gravity.
If the Sun's too dim, build a bigger mirror (it's only metal foil...)
colony at Earth/Moon orbits
colony past Pluto's orbit
edited comment: I checked the book "the High Frontier" about that colony out at Pluto. What the book talks about, is establishing a somewhat arbitrary "continental shelf" for our solar system. They stipulated that an average per-capita energy resource about like the modern US is desired, and then said that they'd limit the mass of the mirror to no more than 2X the habitat (at several wavelengths of light thickness, for metal foil).
The answer came out somewhere like 4 light-days -far beyond Pluto, beyond the heliopause, in interstellar space but well within the Sun's cometary cloud. (plenty of ices out there to live on)
While far out there anti-matter is also an option... However, producing it difficult (and expensive) and contaning it is next to impossible (and very, very expensive).
Yes, that Penn St. article covers antimatter pretty well.
Specifically, it's another form of nuclear pulse (Ion beam Compressed ANtimatter, or ICAN is another name), where pico-grams of anti protons are injected into a HEU target to induce micro-fission/fusion via production of neutrons.
The articles state that only a few milligrams of anti protons are needed for the entire mission (~500 tons in LEO puts a few hundred tons to Mars on a 45 day trajectory. ~120 km/sec delta-V!).
The amount of anti protons is entirely within reason; modest improvements in what we do today would make the entire mission's fuel in 1 year, so we only need ~18 month storage (for a 6 month duration mission; increase this by any surface exploration time past 30 days...), and they talk favorably about improvements in Penning traps & storage devices.
... Lifting and accelerating large amounts of matter into orbit requires a set amount of energy. You can change the timeframe on which this is released but you can't change the amount. Anytime you assemble this amount of energy in one place you must also consider the risk that it might accidently go off...all at once...you have to be careful that you don't blow...your launch pad...off the map.
...You also have to find a way to deal with the wasted heat this will build up on your rocket. Unless you want it to melt, which you probably don't...
In any case, it's interplanetary applications where this is used, instead of getting to LEO.
I like the Sea Dragon for lifting things up (an entire ICAN or Orion ship lifted up to where it can fire the nuclear engine, for instance), but the Shuttle-C or Ares works, too.
I doubt the claim that a rocket accident would be anywhere like a nuke. Sure, it would ruin the pad, but nothing like a nuke. Remember that the Challenger 7 (some of them, anyway) survived the failure & breakup of their booster. Rocket fuels are prone to violently releasing energy, but not quite like an explosive.
(Sure, Zubrin never uses hyperbole, sarcasm, and off-bit humor...)
Actually, a bigger concern is environmental impact of a booster malfunction. That's several thousand tons of kerosene sitting there!
Better yet, buy/lease a disused oil rig, and build your launch facilities on it. Supply it via tanker ships.
Extra benefit of not being on any nation's sovereign territory...
Not dead yet. Posts sent on Sept 3, 4, and 5. I just can't get back as often as I might wish.
What does "Mars floor" mean?
"Phobos" wrote
> On top of that, with in situ propellant
factories and greenhouses on the surface, food,
fuel, and maybe water could be provided to the
spinning space station from Mars itself.
Not upwards. Upwards travel is difficult. If a resource is in hand on the planet, it's more valuable there, to be used for supporting exploration. Resources needed by the space base/hab are much more easily gotten in space, from space resources. As I said earlier, it's inconceivable that Martian reources could out-compete space resources.
Far more likely for a while, that the line would point downwards, with activities on the planet consuming stuff made in space. Any long-term base on the planet (where explorers might base from, during their tour on the surface) would certainly have fuel production, water if possible, but it's more likely that processed items (food maybe) would be dropped in from the space facilities.
> I think once enough habs and people have
been sent on the red planet something like this
won't be out of the question.
Why not at the start? is my point. Install the space infrastructure and profit making base ASAP.
Have profit flowing back into it and a livable hab (Fully shielded and full G) within a year of starting activity at/around Mars.
Send hardhat types first, to establish a habitable base and income immediately, then worry about bringing in dedicated trained explorers to crawl around turning over rocks. ("habitable base" meaning that people can live there with absolutely no concerns about radiation & gravity adaptation, and people on the surface are never more than a few hours and only a few km/s away from support)
We're getting pretty far out here. 3, or 8 HLLV launches to do a single mission? That's a lot of funding to get up front, before a single thing is actually done.
Part of why Mars Direct is small is to keep up-front costs down.
I have another controversial option, if we're thinking of a mission of this size.
Earlier here, the hysteria over launch of Cassini was mentioned, and the 100kw nuclear reactor mounted in a truck.
If you can get past the hysteria to launch the truck, if you can get past the horror stories to launch a nuclear thermal rocket upper stage, then why not go all the way, and use a real interplanetary rocket?
If you're tralking about launching more than a few hundred tons into LEO before the mission starts, and assembling the ship in space, then do it right.
For 500 tons in LEO, you can get over 200 tons of cargo to Mars, in a 6week trajectory! Forget about all the problems with long-term space travel. Forget about cutting safeties & redundant systems to shave off vehicle weight -build it like a Navy cruiser!
So, granted, we'll run into lots of trouble, trying to get variances to the treaties, and then getting the weapons grade fissionables, and setting off a few hundred atomic bombs. We are talking about an enterprise with enough clout to get private funding to do a manned Mars mission... Granted, some protestors will still complain about "polluting space" with the bomb fallout!
Orion at Mars, releasing lander
10 meter Orion upper stage module for S-1-C launch
configured as Mars expedition
Launch profile (if a single HLV-lifted mission is allowable, otherwise, lift separate ~100 ton lots.)
Another aspect of the political difficulties is presented here.
Note that the CDI is not hawkish. They aren't promoting the militarization of space, and certainly not relaxation of weapons-testing or development restrictions.
Orion will rise!
http://www.cdi.org/russia/johnson/5550-12.cfm
Orion Can Rise!
http://www.skali.com/index.p....n=print
...Orion spacecraft was never built. But it offers a radical solution now for using up the thousands of nuclear weapons Presidents Bush of the United States and Putin of Russia agreed to mutually destroy...
It would then be assembled (in orbit) outside an already-existing manned space station.
Such a project would achieve several major ends simultaneously.
First, it would remove from both the U.S. and Russian governments the nightmarish, literally never-ending task of guarding forever the nuclear raw material stockpiles from the bombs they had dismantled. And it would obviously also vastly lessen the risk terrorists like Osama bin Laden or the leaders of rogue states like Iraq or North Korea could steal such weapons or material.
Second, an Orion program would reassure both the Russian and American governments and their publics both sides were indeed handing over their nuclear weapons and eliminating them because those bombs would be needed to fuel Orion space ships.
And with each detonation to provide the kinetic energy to propel the Orion spacecraft further and faster on their voyages of exploration, it would be absolutely certain another genuine nuclear warhead had been destroyed. No huge and flawed program of mutual or international inspection would be required to ensure compliance.
Third, such a visionary program would truly bind the American and Russian peoples together in friendship and partnership. Former House of Representatives Speaker Newt Gingrich, one of the most visionary U.S. political leaders of the past decade, has envisaged a similar constructive unifying goal for the United States and the nations of Western Europe. He has advocated having them cooperate jointly on a manned mission to Mars over the next 20 years.
But Orion would be far cheaper in research, engineering and construction costs than a Mars project using vast numbers of far smaller and slower rockets with outmoded chemical fuel technology. Gingrich's Mars proposal would serve no strategic purpose such as the mutual destruction of U.S. and Russian nuclear weapons. And it would only serve to bind together U.S. and European nations which over the past half century have appeared far less likely to come in to conflict with each other than they all have with Russia.
Finally and fourth, the United States and Russia would prove natural partners in such a project. Both nations have enormous nuclear stockpiles. They have the longest traditions and experience of space flight, exploration and technology by far in the world. And their specializations in these fields complement each other.
We have all this Pu sitting around. What are we going to do with it?
Why not blow it off into the solar wind, once & for all?
Every aspect of this calls for international cooperation,from dismantling the warheads, to flying the Mars mission. Hey -if China gets manned spacecraft flying, the US and Russia might be scared enough to push for the treaty modifications and using Orion for a multinational Mars mission.
Didn't see some other bugs with Mars Direct.
1) no escape system on the crew launch. Better to wait an orbit or 2 for the crew to meet the hab in LEO from a Soyuz or 2, than risk the roman candles with absolutely no hope for survival.
Read here about the Shuttle's rotten safety.
In October 1999, former astronaut Michael Coats testified at congressional subcommittee that he personally experienced sitting on the pad during STS-41-D in 1984 while a hydrogen fire was burning below him and knowing he had no way to escape. Only one month after the release of the NASA safety report justifying not having a crew escape system, NASA had to scrub the launch of Space Shuttle Atlantis because of another hydrogen leak. This time there was no fire and no crew on the vehicle. The gambler was lucky this time... but what about next time..
So use Energia or something without roman candles as a first stage. Plenty of ways around it. (Sure, the crew acccepts the risks, but I doubt anybody is selfless enough to risk that, when there are ways around it)
2) No experience with long term exposure to low G. Much is made of Shannon Lucid walking off the Shuttle after a long time on Mir, and other cosmonauts surviving even longer durations. Yes, they made it, but a decade later, they still haven't completely recovered.
I suspect that .38G for 3.5 years will make the crew either permanently crippled or long-term debilitated after they get back. It'll take far more than mice in orbit for 50 days to settle it, and I suspect that it will prove that low G is almost as bad as zero G. (I've got a couple of long-term bets on it) Face it: people who don't get much exercise just aren't as healthy. They'll have to exercise strenuously for several hours every day of a Mars Direct mission, and they'll still have serious long-term health problems.
Not saying this is a mission killer. There may be other data out there, and you may find a crew willing to do the mission. It is a big unknown, though.
Cheaply copied links, supporting the idea
I've become attached to a few ideas I've found. ASAP build a spinning 1G fully shielded hab in Mars orbit. Make it possible for crews to stay long-term without any health effects, build up to more crew, with more equipment and landers and fuel depots, allow extensive telerobotic exploration of the planet while crews are rotating in & out.
Above all, provide some means of profit... Water! Other chemicals, and easy transport back to Earth orbit -and buyers. (none of this is mine: "Plagiarism is copying from one source, while research is copying from many sources".)
The Diemos Water Company article points out the benefits of going to Mars' moons.
See also the book "Mars 1999" by Brian O'Leary. He suggests that the first Mars mission goes to the moons first, to make fuel and establish the base/chemical extraction factory before comitting to landing. The first and every crew carries a tank of water back to LEO when they return. (O'Leary used the phrase "Ph&D" for Mars' moons)
See the Bootstrapping space industries article by Bruce Mackenzie. Note especially his spinning station/depot design, and the emphasis on bootstrapping. Ideal for the Ph&D orbit Mars base.
This one can't be over estimated
Projects to Employ Resources of the Moon and Asteroids Near Earth in the Near Term
http://permanent.com/
I think it answers many ill-informed objections about space processing, space industries, etc. There is literally tons of info out there on space processing, and for evey doubtful part of a process, there are several other ways which would work.
Near Earth Object Fuel (neofuel.com)
Maybe also to the point here, is this:
http://members.aol.com/oscarcombs/spacsetl.htm#zubrin]
Didn't Robert Zubrin debunk this whole SPS/space settlements scenario in his book "Entering Space"?
from the Space Settlement F.A.Q.
Transplanting a sub-topic which started budding off in the "Energy Transfer" topic, this seemed to need discussion of its own, as a new sort of mission architecture.
Note the links I provided in that thread, as a background for why I feel confident with this proposal.
I don't know if the doom and gloom over 0.38G is justified
I don't either. I do know for a fact that it's far safer and more conservative to say that we do know for a fact that we can fairly easily provide full G for the crew, and that they'll be entirely healthy in it.
Nothing of the sort can be said for low G, and it'll be a long time before we're certain -a long time of space missions to find out, unless you're able to find a crew to volunteer to be highly paid for the remainder of their lives spent in therapy to regain their health. Even if they're not physically ruined by the long exposure to low G, they don't know if they will be, before they launch. You're going to have to pay them very well for the gamble, and run the risk of being known for using up a crew just for impatience and not being willing to do your homework.
This started when I talked about a modicum of space infrastructure around Mars' moons being better than dropping exploration crews on the planet, with no attention paid to space industry.
Mars Direct leaves in place a network of safe havens and exploration gear on the planet. This is great for exploring the planet, but a little effort on Ph&D does far more. Near-term profitability is the big one. Get tanks of water or other chemicals back to EO, and the missions are paid for right away, along with bankrolling the future of the Mars effort.
The infrastructure of the water factory at Ph&D is easily built up to a more complete factory (In the same timescale as 3-5 Mars Direct missions, let alone building any sort of semi-permanent base on the planet.)
Cable & rock dust for concrete (shielding and structure in one piece, far more robust and actually cheaper than the alternatives), and rolled & stamped metalsfrom sapce resources are used to build a base from tools & finely machined parts brought from Earth (Zubrin pointed out the difficulty of making something as small as a screw & nut; we bring along screws, and make the dumb bulk beams out of moon dust).
Settle for .38G on the way out, but the same habs are built up at the base, with extra truss length and strength for spinning newly shielded habs for full G.
The base isn't mass sensitive, so we build the bulky parts of the base from materials easily gotten in space, from the skeleton delivered by the transit habs.
Graphically showing my point, first for low G, unshielded habs:
habs = 5-15 tons, spin cable = ~3tons
now for Full G, shielded habs
habs = 750 tons, truss = 2500 tons
(SWAG, for ~Mars Direct sized habs. Feel free to pick the asumptions apart, but I doubt the picture gets any better than this.)
Far easier to bring along tools to build the larger habs from moon dust, especially since the same infrastructure provides profits for the Mars effort, as well as a strong support base for the exploration of the planet.
Now we've got fairly early sustained funding for the Mars effort, and completely livable conditions for long duration crew stays at/around Mars.
Shaun Barrett wrote
> I and a lot of other people happen to be very
fond of the idea of "simply plopping" them down on
Mars! .... and the sooner the better.
I agree. Shooting off Mars Direct missions is the ideal thing for now. I can't think of anything as possible in the near-term which would mean as much as this.
I have no problem with a crew of only 4, and letting them take their risks and the glory when they get back.
Only 2 particulars bug me:
1) no escape system on the crew launch. Better to wait an orbit or 2 for the crew to meet the hab in LEO from a Soyuz or 2, than risk the roman candles with absolutely no hope for survival.
Read here about the Shuttle's rotten safety.
In October 1999, former astronaut Michael Coats testified at congressional subcommittee that he personally experienced sitting on the pad during STS-41-D in 1984 while a hydrogen fire was burning below him and knowing he had no way to escape. Only one month after the release of the NASA safety report justifying not having a crew escape system, NASA had to scrub the launch of Space Shuttle Atlantis because of another hydrogen leak. This time there was no fire and no crew on the vehicle. The gambler was lucky this time... but what about next time..
So use Energia or something without roman candles as a first stage. Plenty of ways around it. (Sure, the crew acccepts the risks, but I doubt anybody is selfless enough to risk that, when there are ways around it)
2) No experience with long term exposure to low G. Much is made of Shannon Lucid walking off the Shuttle after a long time on Mir, and other cosmonauts surviving even longer durations. Yes, they made it, but a decade later, they still haven't completely recovered.
I suspect that .38G for 3.5 years will make the crew either permanently crippled or long-term debilitated after they get back. It'll take far more than mice in orbit for 50 days to settle it, and I suspect that it will prove that low G is almost as bad as zero G. (I've got a couple of long-term bets on it) Face it: people who don't get much exercise just aren't as healthy. They'll have to exercise strenuously for several hours every day of a Mars Direct mission, and they'll still have serious long-term health problems.
> I wish it were as 'simple' as you make it sound.
I never say it's simple (I do say that it's not as hard or expensive as the government makes it look). It'll cost lives, several tens of billion$ to start, and a decade or more to show any promising sign for the public that the expense isn't wasted on "flags & footprints", and maybe some stuff being moved around.
I've become attached to a few ideas I've found. ASAP build a spinning 1G fully shielded hab in Mars orbit. Make it possible for crews to stay long-term without any health effects, build up to more crew, with more equipment and landers and fuel depots, allow extensive telerobotic exploration of the planet while crews are rotating in & out. Above all, provide some means of profit... Water! Other chemicals, and easy transport back to Earth orbit -and buyers. (none of this is mine: "Plagiarism is copying from one source, while research is copying from many sources".)
The Diemos Water Company article points out the benefits of going to Mars' moons.
See also the book "Mars 1999" by Brian O'Leary. He suggests that the first Mars mission goes to the moons first, to make fuel and establish the base/chemical extraction factory before comitting to landing. The first and every crew carries a tank of water back to LEO when they return.
See the Bootstrapping space industries article by Bruce Mackenzie. Note especially his spinning station/depot design, and the emphasis on bootstrapping. Ideal for the Diemos orbit Mars base.
This one can't be over estimated
Projects to Employ Resources of the Moon and Asteroids Near Earth in the Near Term
http://permanent.com/
I think it answers many ill-informed objections about space processing, space industries, etc.
Maybe also to the point here, is this:
Didn't Robert Zubrin debunk this whole SPS/space settlements scenario in his book "Entering Space"?
http://members.aol.com/oscarcombs/spacsetl.htm#zubrin
well lessee, so far i`ve heard 30 bil, 50 bil, & now, ca ching 10 bil.
In private, it can be speculated that a mission could be done for even less. Maybe 5 bil or even 2. This is the price of the hardware at rock-bottom, with no inflated overhead, no mistakes, no fat. Who knows if this includes pay for the crew and everything else which goes on during the mission.
They say an elephant is a mouse built to government specifications. I'd say a diplodocus is the NASA version.
* Remember that McDonnel Douglass & the BMDO build the DC-X vehicle testbed in 6 months, for under 60 million. (that's million)
* Rutan & Scaled Composites built the Voyager (Round the world unrefueled airplane) for something like $3 million. Estimates for the typical government aerospace/defense contractor cost would be more like $150 million.
* Just after the start of Desert Storm, the USAF put out a request for a earth-penetrating "Bunker Buster". Less than 1 month later, the GBU-28 saw combat action!
OTOH, there's the example of the "Space Pen":
During the early days of manned spaceflight, they had to come up with a way to let astronauts take notes and mark checklists in space -in zero-G, ink won't flow down to the nib of a pen.
They spent $70 million, and developed the space pen. It's amazing: Writes upside down or in zero-G, writes under water or bleach or oil, writes on glass or anything else.
The russians used a pencil.
At the first Mars Society convention, former Gemini & Apollo astronaut John Young gave a talk. I don't remember what his topic was, but he glanced past solar panels.
The solar panels on Mir or Skylab or most satellites are great; Unfold them, point them at the Sun, and you've got power.
He said that the ISS has solar panels, too. Do you know what they need to produce power?
Software.
First of all, this newest space initiative doesn't include anything at all for nuclear thermal. Only fission power systems to power probes and possibly NEP thrusters for outer solar system exploration. Nothing big enough for manned ships, at that.
One reason for this nuclear initiative is that there is only one single RTG stockpiled for space probes, of an old design. This new program modernizes the designs, and builds more.
This probably means that there's not much there for VASIMR either. That plasma thruster is very power hungry, so it would take big nuclear power plants -far bigger than anything flown to date.
I doubt the value of VASIMR anyway. The same performance can be achieved with far less expensive R&D with nuclear thermal: First, VASIMRs designers say its variable thrust/isp allow it to thrust all the way there, vastly shortening the trip times.
Everything they claim has been either tested or planned for NTR for a long time.
First, for low-efficiency big thrust (for liftoff from Mars or the Moon or perigee-kick propulsive maneuvers) there's the O2 "afterburning" NTR. Inject O2 into the exhaust stream of an NTR, and the exhaust cools, EV and isp drops, while thrust goes up.
This gives equal capability to VASIMR, with far less new technology needed (No supercunductors or plasma handling).
Second, NTR can equal the performance of VASIMR in the part of the flight where VASIMR throttles down, for low-thrust, long duration, high efficiency travel.
Shut off the rocket, run coolant through the pile into a power turbine, for a closed cycle power plant (designed by Pratt & Whitney) to power ion thrusters (already extensively tested, and flown).
This dual mode (really triple mode) NTR can do everything VASIMR claims, with everything involved relying on well known, tested or even flown equipment.
For the real kicker, the performance cited for VASIMR (3 months to Mars) can be beaten with an even earlier, well known (if unpopular) method.
The 10 meter, HLV boosted Orion engine module gets a ship of a few hundred tons to Mars, ~45% of the mass being cargo, on a 6 week trajectory. This was 1960s technology... simple, dumb, and supposedly as cheap as the booster to get it off the ground.
If "clean" bomblets can be made for the low altitude part of the flight, then we've got hundreds of tons to Mars in 6 weeks, with one HLV shot. (compare that to Mars Direct! It even inlcudes an escape module for the crew during launch, unlike Mars Direct...)
If the "clean" bombs can't be made, then we take 5-6 launches to do the same thing. Unfortunately making the mission that much bigger, and requiring space assembly, but for what a ship!
Byron wrote:
... another consideration is public opposition to microwave energy being beamed down from space...what if the powersat shifted slightly, and all those microwaves accidently cooked a city or whatever.
Forget about it. The beam for an SSPS system is about 1/10 the intensity of sunlight, and it's also in a freq which won't affect anything smaller than ~3 meters (a significant fraction of the wavelength). Buildings will be immune, as will people, airplanes, birds, etc.
Since there won't be any cheap carbon-based fuels to burn on Mars, solar and nuclear (and hopefully geothermal) energy will be the way to go on Mars
Surface-based solar is limited by nightfall. Nuclear must be imported and soft-landed from Earth. Mars seems to be tectonically dead; Not enough geothermal heat to warm much more than a small pool of bacteria (hopefully, and that probably not near where we'd like to build a big base)
... if the initial infrastructure of mirrors and collectors could be financed and constructed, it would greatly reduce the amount of energy that would have to be produced on the surface through the use of nuclear power plants or whatever.
Go to Mars' moons, and finance the entire thing -including future Mars exploration by extracting water for shipment to Earth orbit (the answer to quesations about self-financing Mars exploration).
Build SSPS in Mars orbit, send down materials to roll out rectennae, and have ample power anywhere on Mars. Build the long-term Mars base in orbit, and have fully shielded, full Earth gravity habitation at Mars (which you can never have as easily on Mars itself).
Just keep in mind that it's always going to be more costly to build anything in space as opposed to on the ground (even the Martian surface)
Says who? I can point to lots of other studies which show exactly the opposite.
Get resources from an asteroid or Mars' moons, get any amount of energy you need from the Sun, move tonnages around cheaply, build large things fror use in space, or to be packaged for delivery to the surface, etc.
Tom Jolly wrote:
I've always thought SPS was a dumb idea. No matter how efficient you can make it, you can take that same efficiency and employ it on Earth's surface to collect sunlight without any launch costs and with easy access for repairs and replacements. Granted, you might only be functional for 8 hours a day, average, but who cares? The cost per watt to build the thing is a hundred times cheaper
Right there is where most detractors of SSPS go wrong. Don't forget that the Space industry system is going to be self-financing after not too long (if it's not, then it won't be built) Asteroid metals are a big one, Geo-synch telecommunications arrays are the other: huge antennae and huge areas of solar power collectors will let a few stations cover the entire planet, and pick up a cel phone from the grond. All this will take is wire, concrete, and rolled & stamped metals -all easily produced in an early space manufacturing facility.
Fully 95%+ of the facility and the antennae farms are built from bulk space resources.
Bootstrap the capability, instead of the stupid idea of lifting an entire factory from the Earth -using the even more stupid idea of lifting the entire thing with the Space Shuttle! Here's one: "You want to build a city on Mars? Figure the city weighs a billion tons, and you have to lift it on the Shuttle. Then you have to lift all the chemical fuels to boost it to Mars, and soft land it on Mars, and your Martian city is clearly impossible"
That's the kind of modelling some (unnamed) people use to detract from the space industry concept.
...besides the fact that it's totally uneconomical
only if you use the worst possible (or impossible or at least unlikely) assumptions. Change your models, and the entire outlook turns about.
... it would also increase the incident energy arriving on Earth, where ground-based panels wouldn't...
Earth-based solar requires Earth-based industry; space industry eventually involves no pollution in the biosphere whatsoever! The only effect on the biosphere is the incident energy from the power beams. All other energy intensive and heavily polluting industry is done off-planet...
And that is the part where the potential of space infrastructure and SSPS comes out on top. (Not to mention it stops the need to burn oil, adding to the greenhouse; killing another of the straw men erected to argue against space industry & SSPS)
Not just a multi-planet species, but a space-faring species. Not just crossing space to drop down into another hole, but living in all of space. Far more than just one more tiny planetary surface to expand into.
Far more important to the long-term survival of the species and Gaia than simply plopping tuna cans down on Mars.
I wrote:
Somebody mentioned fusion only (nuclear explosives).
We've got to convince the DOD to declassify some
of their new R&D for such things. If we could
guarantee that there are no long-lived isotopes
-or short lived but highly radioactive ones which
may be worse-, would it be such a problem?
There's some debate over whether this is possible today. I don't pretend to know, but it is interesting.
Somebody once suggested neutron bombs to me: No or very little lingering radioactivity or fallout sounds like exactly what we need. The prompt pulse of neutrons from a 84km altitude string of blasts of only .1kt ech, over the middle of the ocean coudn't hurt anything. Eliminate the enhanced neutrons, but keep the "clean" nature, and we're more than halfway there. Eliminate the gamma rays, and what little fear of EMP there is from such a tiny blast also disappears.
Take these to the extreme, and maybe a Big One could be ground launched.(?) That's a dream-prospect: 10,000 tons at liftoff, more than 50% of that being cargo to Mars on a trip of less than 2 months...
If you can't accept the possibility of making
clean bombs, or even the acceptabillity of such
zero-impact launches politically (if possible),
then there's always the hard way. 5-6 Ares
or Energia launches does it.
Lift the parts to LEO to be assembled. I like the ability NPR gives to mission designers to build parts massively. Think of a typical merchant ship -if not a battleship- rather than a fragile aerospace construction. Simple, dumb connections could hopefully eliminate much of the difficulty of EVA assembly work.
Send the Pu pits for the pulse units (bombs)
up in a separate launch, with tremendous care
taken to preserve & protect the Pu in case of a
launch accident...If the booster malfunctions,
the Pu itself is preserved as well as a crew
would be!
The version of the Shuttle-C with 2 SSMEs on the cargo pod is arguably the cheapest near-term booster we could get. It puts ~40 tons into LEO. This allows for some pretty robust packaging. If this isn't enough, the Ares puts ~120 tons into LEO, or ~65 without the upper stage.
I think we can practically guarantee that the plutonium bomb pits could survive, and be readily recovered.
Use ED tethers or something to lift the apogee
above the Van Allen belts before the NPR
engine is fired.
This points out another way that the immense capability of NPR simplifies things: You don't need to scrimp propulsive effect by firing the NPR engine at perigee (the closest approach to Earth) for the best effect. Go ahead and fire it off while at the weak, lowest velocity (highest altitude) portion of your elliptical orbit.
Really, the performance available from this engine changes your way of thinking about spaceflight.
the propellant to be vaporised by the blast and
directed at the ship's pusher plate is ~90% of the
mass of the pulse units.
This from a quote from Dyson, while discussing water resources in space. The (rough) figure of 45% of the IMLEO being cargo at Mars doesn't include this capability. Eliminate 90% of the mass of the return delta-V "bombs", and fill up with Diemos water, CH4, NH3, or whatever ices are most handy (It arguably being easier to get at such resources at Diemos than on Mars itself)
"Phobos" wrote:
... I do like that idea of using a tether though
to lift a nuclear rocket up into a safe area
above Earth. With properly encapsulated
nuclear explosives there'd be very little danger
of nuclear material being leaked into the
environment if the tether were to snap.
Or nuclear or solar thermal. whatever works (ED tethers are nice because they're a workable version of "magic" propulsion -no propellant mass being thrown backwards!)
I'm not entirely sure we understand each other in mentioning tethers.
First, you cannot use tethers to lift 100 tons, or even 20 tons from the ground... We still are stuck with chemical rockets for that. I doubt ED tethers are even strong enough (with reasonable mass/thrust ratios) to lift from a sub-orbital trajectory before it re-enters on the other side. (If a first stage gets something to orbital height, but not quite enough velocity, then 1/2 orbit later the perigee will be too low, and you lose it. A spinning tether can exchange orbital velocity with a comparatively much smaller load, raising the load's perigee above the atmosphere.)
A momentum exchange tether station could concievably do it in one throw, but if you can build, launch, and operate one capable of lifting a 20, 100, or 500+ ton load from a hypersonic suborbital trajectory to a high orbit above the magnetosphere, then you don't need anything else, because you can work miracles.
You must get your load into LEO, and extend solar panels or fire up a nuclear plant to power the ED tether, for a gradual boost, probably taking days.
You wouldn't have to worry about a chemical
rocket exploding and potentially spreading all of
those little bomblets all over the Atlantic.
Forget about vaporizing the bomb pits, even in a worst-case accident. If the packaging split, spilling the bomb pits or complete pulse units, they'd fall harmlessly to the bottom of the ocean (they are extremely dense, well built objects, and they wouldn't be broken up in a typical launch accident)
If it's a one-HLV launch, with the NPR engine being fired at the top of an arc, the bomb pits are in the middle of a 580 ton chunk of ship, so they'd be recovered intact from the wreckage at the bottom of the ocean. We'll package them to survive if they're cargo on a booster (in the case of a multiple HLV boosted, LEO constructed ship.
Sure, we have examples of RTGs burning up and spreading radioactive debris. I'll argue that they weren't designed properly...
These were not launch accidents, but re-entering satellites. By definition, a booster acident involves much less energy, and properly designed RTGs would be intact at the bottom of a hole in the ground, even if falling from orbit. (Yes, a booster malfunction involves lots of energy, but very little of the energy of a rapidly burning cloud of rocket fuel goes into the payload. Comparatively, falling from orbit is more stressful...)
Anything threatened by radioactive leakage would already be crushed by this dense mass falling from the sky!
A water tank from Skylab survived orbital re-entry mostly intact.
The crew of the Challenger survived the booster malfunction and vehicle breakup. They fell for 2.5 minutes, and the impact with the ocean is what killed them (no parachutes, airbags, or basically any kind of survival possibility on the Shuttle).
Hitting the water is something a properly designed container could survive. (Especially if we launched the pits in a recoverable "escape module" with parachutes, airbags, or the sort. Plutonium is valuable enough to go to the effort.) Booster malfunction, fuel mass-combustion, range safety charges, and all, we could ensure the safe recovery of the bombs (easier than people!).
An Ares boosts 120 tons to LEO, or ~65 tons without the second stage. The 2SSME variant of the Shuttle-C is the cheapest, nearest term HLV we could get, and it lifts ~40 tons, so that means 20+ tons of protective packaging for the bomb pits.
(C M Edwards @ May 12 2002)
Nuclear fission pulse rockets, however, _are_ supposed to leak. Everything I'm leary of nuclear thermal rockets because there's even a slight risk they might do, nuclear fission pulse rockets do as an integral part of their operation.
Pretty much correct. NPR was designed to get around the materials limitations on NTR, posed by the melting point of the engine's structure. No effort is made to continually confine the plasma of a nuclear pulse engine, thus much more of the energy of nuclear fuels can be used. At this, only a tiny fraction is actually used. The horrendous efficiency can be excused by the fact that they're using nuclear fuel in the most energetic way possible -a runaway chain reaction blast.
I could stand some convincing about NERVA. But if anyone ever proposed using a nuclear Orion system for Earth launches, you would find me among the protestors chained to the launch pad.
Briefly exciting, but they won't find much of you -or the launch pad!
Let's look at this: What are the problems with it?
They figured that their full interplanetary exploration program (not just one ~10,000 ton ship launch, but several) would add a few percent to what we were already adding to the atmosphere with weapons testing.
Still, we don't want to do even this.
Somebody mentioned fusion only. We've got to convince the DOD to declassify some of their new R&D for such things. If we could guarantee that there are no long-lived isotopes -or short lived but highly radioactive ones which may be worse-, would it be such a problem? Launch from an expendable floating platform at sea, where there's no surface dust, and we've got thousands of tons to orbit in one shot.
Another option is the "second generation" Orion: what they designed for an upper stage for a Saturn S1-C booster.
Freeman Dyson is reported to have felt that this restriction lost much of Orion's appeal -the Saturn booster would have been over 50% of the cost. (Now this probably meant the currently selling government graft system costs for the chemical rockets, versus the cheaper, reasonable, zero-graft costs for the Orion stage.)
Nevertheless, This puts 500 tons into LEO. If cleaner bursts can be made for the lower portions of the flight, where some exhaust products (a few grams maybe?) might enter the atmosphere, then we've got a tremendous lift capability for each Energia or Shuttle derived launch stack.
There is arguably nothing else we can design -even today- that's as near-term, and any where near as capable as Orion.
This single-HLV mission was for an 8 person crew, with a 6 week trajectory! ~45% of the mass in LEO is cargo bound for the destination!
This capability removes every major stumbling block on the way to Mars, or indeed the rest of the solar system.
Long duration spaceflight dangers will be a thing of the past.
If you can't accept the possibility of making clean bombs, or even the acceptabillity of such zero-impact launches politically (if possible), then there's always the hard way. 5-6 Ares or Energia launches does it.
Most "traditional" Mars missions call for some hundreds of tons in LEO. The difference is that with this one, the cargo is the bulk of it, while with chemicals, 90% is fuel.
Send the Pu pits for the pulse units (bombs) up in a separate launch, with tremendous care taken to preserve & protect the Pu in case of a launch accident. This is as much to satisfy people against the preachers of fear of such nonsense as "vaporising the Pu and spreading billions of doses of cancer across the entire planet", as it is to safegard the valuable resource. If the booster malfunctions, the Pu itself is preserved as well as a crew would be!
(the propellant to be vaporised by the blast and directed at the ship's pusher plate is ~90% of the mass of the pulse units. This makes for maybe ~20 tons of Pu itself)
Another idea is the Truax Sea Dragon: the entire 500 tons ship into LEO in one shot. Use ED tethers or something to lift the apogee above the Van Allen belts before the NPR engine is fired.
Long term, Nuclear pulse is arguably the solution for interplanetary travel. If inertial confinement-type fusion engines can be made, then fine, but we know that there's U in asteroids. Any metal mine on an NEA will uncover it, and we know that there must be planetary masses of asteroids out there. Industry in space will allow for huge rapid travel ships (The bigger you make Orion, the better).
Weeks to Mars or the asteroids, months to Jupiter and its moons & trojans, with robust, comfortable & safe ships and massive cargoes.
10 meter upper stage module for S-1-C launch
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configured as Mars expedition
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Launch profile
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Visited by moderator 2022/02/02
> Getting from Earth?s surface to Earth orbit requires
a great deal of power as well as energy.
>...
> Does that leave us stuck with chemical rockets
forever? Are there any alternatives for Earth launch?
Lightcraft are one. Up to the old ideas for flocks of 2 ton pods to a given LEO spot every 90 minutes or so. With a little bit of rocketry to circularize, they'd be a wonder.
Further advancement is offered by tethers.
They'd make a great upper stage either for a payload tossed up by something like a rocketplane or laser-thermal, or to lift the entire craft to LEO, as in the Hypersonic Skyhook. (Neither of these options is to be mistaken for the magic Beanstalk or synchronous skyhook. Momentum exchange and the
are obtainable with today's materials.)
Frankly, I'm not too dismayed to be stuck with chemical rockets.
With only limited advances, we could revolutionise space access -if we revolutionise our book-keeping and procuring practices: Do NOT buy parts through government graft & contractor lobbying. Day-to-day space access should be privatised, and we'd see a marked decrease in cost.
If the Mars Society gets a mission going, then they'd provide this: Opening production lines and procurement practises for business and private interests without paying government overhead would be one of the greatest gifts the Mars Society could give to humankind!
To nuts & bolts, we all know about the Ares.
The Shuttle-C
is even more near-term, because the ET is unchanged; the only change is to toss the orbiter over to the side of a hangar somewhere. Next, get rid of the roman candles, in favor of
liquid strap-ons.
The Shuttle Orbiter isn't very good for crew launch anyway (it's manifestly unsuited for heavy lifting) Use Soyuz, or evolve to using something like the old HL-
http://www.astronautix.com/craft/hl20.htm]20
http://www.astronautix.com/craft/hl42.htm]42
Notice that one of Grumman/orbital Sciences' proposals for the new NASA SLI is this older spaceplane. (Scroll down to the N-G/OSI section).
Costs would drop, but safety & assured crewed access to space are paramount. (One of my problems with the Mars Direct is launching the crews on top of the booster, without even the Shuttle's unlikely possibility for escape.)
For another idea, there's the old Truax Sea Dragon proposal. 500+tons to LEO in one shot, cheaper than a Shuttle by far.
Just to show that re-usability isn't necessarily the way to lower costs.
Of Course, it would be nice to have an airplane you step into, it rolls down the runway, and takes you to orbit. (The old dream...) The Devil is in the details, of course.
Airbreathing is about the only way, which for now means jets of some sort. Eventually, they'll learn to make SCramjets, which will help, but for now, it's multiple engines for different regimes of flight.
Work on something like the Russian tripropellant rocket engines would be a step in the right direction, too.
For the true spaceplane, we almost need nuclear thermal for the upper stage portions of flight -where rockets would kick in. It may someday be possible to make a NTR airbreather (and make it safe enough that there wouldn't be hysterical fears of a "Chernobyl-like disaster"), but that's way out there.
For that matter, O2 afterburner NTRs would help, too. Increase the thrust, at the expense of some loss of EV, exhaust temperature, and ISP for the O2 being thrown out. Does that change the outlook for NTR spaceplanes?