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#76 Re: Interplanetary transportation » Space Elevator or Scramjet? » 2007-11-28 06:47:23

The problem with a mass driver isn't really the air friction. You'll puncture through the thick part of the atmosphere so damn fast you won't really have time to heat up. At escape velocity you'll hit the stratosphere in a second and the mesosphere in less than 5 seconds. T+8 seconds you'll be out of the mesosphere and out of the danger zone. So if the heat shields can hold out for a mere 8 seconds, you're golden.

The real problem with mass drivers is the enormous g-forces required for them to work. There's just no feasible way to ever man-rate them on Earth, unless we manage to build a space elevator and run an acceleration rail along it.

Mass drivers will primarily be of use to deliver materials that are very resistant to high (200, 2000, even 20000 g's) accelerations. Meaning, stuff that doesn't have any appreciable internal structure to break. You could use mass drivers to deliver water, gas, raw metals to orbit. People? Never. Anything with a fine structure, such as electronics? Unlikely, but perhaps possible with durable enough components.

#77 Re: Terraformation » Minimal Martian Terraformed Atmospheres » 2007-11-27 09:32:05

Is there any reason they wouldn't become acclimatized in the womb? They do share the mother's blood circulation at that point, after all.

#78 Re: Terraformation » Minimal Martian Terraformed Atmospheres » 2007-11-27 01:10:37

Well, if the only flammable things on Mars are our farms and colonists, then that's what'll burn. smile

Of course, we could plant forests and tundra (?) so the rising O2 concentrations would have something else to burn than our farms and colonists...kind of like providing false targets...

#79 Re: Terraformation » Minimal Martian Terraformed Atmospheres » 2007-11-26 22:15:23

There's also the concern that if you started having plants on a planetary scale, not just in one or two craters, having enough of them, they'd start eating up all the CO2 and soon you'd have an O2 atmosphere which would self-ignite and everybody would die in a firestorm. smile

You could try to regulate the pace of CO2 -> O2 conversion, but we're not even managing to do that here on Earth...

So again, buffer gas, buffer gas, buffer gas. It is the cureall. wink

#80 Re: Terraformation » Minimal Martian Terraformed Atmospheres » 2007-11-26 18:11:16

Figuring out a way to infuse good amounts of buffer gas would pretty much solve all of those problems though. All of those problems more or less just mean, "insufficient buffer gas". That's all it comes down to in the end. We need buffer gas. smile

#82 Re: Terraformation » Minimal Martian Terraformed Atmospheres » 2007-11-26 16:26:03

Nickname, you are absolutely right that we should not ignore the CO2 toxicity.

I think most people are just hoping we'll get huge amounts of oxygen and buffer gas from...somewhere, I dunno, I guess they're thinking of bombarding Mars with asteroids or something.

For humans, building up the pressure is enough, it can be all CO2 if that's what it takes -- we can wear breathing masks if so.

But plants can't wear breathing masks, so if we want to open sky farm on Mars, we'll have to have a lot more gases in the atmosphere than just CO2.

Of course, we could always closed dome farm.

#83 Re: Interplanetary transportation » Space Elevator or Scramjet? » 2007-11-26 16:12:42

Let's assume an ideal best case scenario: a balloon of mass zero, containing a vacuum (the best lifting "gas"). So, neither the balloon canvas nor the balloon contents add any additional weight to the system (as I said, idealized).

International Space Station mass is approximately 230 000 kg.

In order to lift an ISS with a balloon, you would need buoyancy B that is equal to the station's weight W.

W = B
m(ISS)*g = rho(air)*V(air)*g (the gs can be divided away)
V(air) = m(ISS)/rho(air)

If we take the displaced air in spherical shape

4/3*pi*r^3 = m(ISS)/rho(air)
r^3 = m(ISS)/rho(air)*3/(4pi)
cubic root that

Taking air densities at particular altitudes from http://en.wikipedia.org/wiki/Barometric_formula

20km altitude - 0.088 kg/m3 - 85m radius balloon
32km altitude - 0.013 kg/m3 - 161m radius balloon
47km altitude - 0.00143 kg/m3 - 337m radius balloon
51km altitude - 0.00086 kg/m3 - 400m radius balloon
71km altitude - 0.000064 kg/m3 - 950m radius balloon

In real conditions the radius would have to be somewhat larger to compensate for the weight of the balloon canvas and the gas contained within the balloon. But I think it's a close enough estimate to say that lifting an ISS to 70km altitude would require a balloon roughly 2km in diameter. (Or more sensibly of course, multiple balloons with the same volume, to avoid catastrophic failure.)

Incidentally, it would mean pretty much not being able to look (or launch) upwards at all, as pretty much everything above you would be taken up by the balloon. You could only look sideways or downwards. Looking up, anywhere you look is balloon. smile

#84 Re: Terraformation » One crater at a time » 2007-11-26 03:57:27

CO2 has a molar mass of 44, versus O2 of 32 and N2 of 28. So it's not so much heavier that some of it couldn't be thrown higher up in the air by currents.

SF6, conversely, has a molar mass of 146...which is pretty drastically different from all of the above.

I'm not saying it wouldn't leak at all -- in an open crater, everything would eventually leak -- but I think it would be a really slow process, especially if you only, say, half filled the crater to 4.5km and let the top half be CO2. The SF6 would have to work its way 4.5km up through the much lighter CO2.

#85 Re: Terraformation » One crater at a time » 2007-11-25 23:07:05

There's a lot of talk about what a massive undertaking it would be to build up an atmosphere for the entire planetary mass of Mars.

There's less talk about building local small-scale atmospheres. And I'm not talking about domed cities and habitats, but open-sky.

If you flooded, say, Hellas Planitia with SF6, the gas would stay at the bottom of the crater, would it not? By virtue of being heavier than the CO2 atmosphere above it?

Mars is pretty rich in craters, why not make that work for us? Basically, there are a lot of ready-made "cups" that you could pour "liquid" into. The crater rims should serve as natural containers to prevent the (heavy) gases from spilling out significantly. (Light gases like O2, N2, would rise above the CO2 and mix into the planetary atmosphere.)

At 1150 km radius and 9 km depth from rim to bottom, Hellas Planitia for example would fit approximately 3.7E16 cubic meters of gas. Which is still a hell of a lot (and you'd want to practice on smaller craters first) but it is also a hell of a lot less than doing the entire planet.

If you had a 9000m x 1m x 1m pillar of SF6 on top of a square meter of Hellas soil, it would be 9000m3 x 6.164kg/m3 = 55 476kg per square meter. Given martian gravity 3.69m/s2 * 55476kg ~= 205 000 N/m2 = 200 kPa = 2 bar.

(Martian gravity would be trivially more at the bottom of Hellas Planitia but not enough difference to worry about.)

One thing where my calculation is probably wrong is that the density of SF6 should be lower at Martian lower pressures. Calculation help with that?

If you didn't fill it to the rim, you'd reduce the amount of gas loss to the outside by staying away from the border zone, at the price of providing less pressure to the bottom of the crater.

One of those "black holes" we've seen on the surface could also be an interesting target to pour heavy gases into.

#86 Re: Space Policy » Chinese Space Program? - What if they get there first » 2007-11-25 10:10:11

I agree that political correctness and playing it safe have killed mankind's adventuring spirit sometime in the last 50 years. I know I'm going to take a lot of heat for this, but if people dying is what it takes to get us into space, then by all means, blow those people up. I do not regret the people who died in Challenger and Columbia. People *will die* if we want to get into space. Pioneering a new frontier should never be safe, and if it is, then you're just doing it wrong. Look at all the people who died in colonizing the Americas. A new frontier is pretty much unsafe *by definition*, almost. Sure, you can check and double-check and triple-check and quadruple-check everything and have a thousand redundancies to get a near 100% success rate. But by that time, you'll be putting so many man-hours into safety that the program will grind to a halt under all the safety measures.

That's what we've seen in recent decades. We've become so obsessed with safety, afraid of taking risks, that we can't do anything useful anymore. Fear of Challenger and Columbia repeats has more or less paralyzed America's space program.

We're not going to get anywhere by playing it safe. Any person who plays games of chance will tell you that if you take low risks, the rewards will be equally low.

If we want to spend the next 50 years expanding the ISS by 50%, whoop-de-doo. If we want to do anything *meaningful*, we will have to lower safety standards, take bigger risks, blow people up, and get somewhere.

That's my view anyway.

#87 Re: Space Policy » Chinese Space Program? - What if they get there first » 2007-11-25 09:28:40

I don't want to get into an extended Republicans vs Democrats debate on a forum where I want to talk about getting mankind into space, so let me just say that I'm very strongly a democrat, and very strongly pro-space, and I am not alone.

#88 Re: Space Policy » Chinese Space Program? - What if they get there first » 2007-11-25 00:50:56

As somebody who considers himself very liberal and very democratic, and for whom a candicate's space policy is one of the top three reasons to vote for them, I find your characterization inaccurate scapegoating. You're just trying to shift blame on "the other side".

There are just as many ku klux klan rednecks down south who couldn't give a damn about going to space, just about hunting down them thar blackies and seein' em hang.

If we want to mudsling pointless stereotypes, that is.

Don't try to make this into some make-believe "republicans are pro-space and democrats are anti-space". If that were true, why would Bush (a republican of the worst kind) be against NASA funding increases?

Space is something that attracts both right-wingers and left-wingers alike. It isn't political parties that split us apart, but rather, it is something that *unifies* both parties. In this day and age of a split America, we should highly value any such things that are common ground and of interest to both sides.

#89 Re: Science, Technology, and Astronomy » Lighter than Air Suborbital Craft » 2007-11-24 23:03:02

No, I'm sorry. In a vacuum (or near-vacuum), a balloon will fall if it is in a gravitational field. Its lift comes from displacing air. If there is no (or very little) air to displace, it won't have lift.

Buoyancy B needs to be greater than weight G, in order for the balloon to rise. In a vacuum or near-vacuum there is no or trivial buoyancy.

#90 Re: Terraformation » Optimal human living conditions » 2007-10-23 19:36:36

All in all these effects are hard to determine in advance.  The human body is quite adaptable, but to truly get a good idea of what living conditions are "optimal" you would have to do some long term studies on largish population groups.

Oh, absolutely, but I'm not asking for *knowledge*, I'm just providing a springboard for some fun speculation.

Speculate, go nuts. smile

#91 Re: Terraformation » Optimal human living conditions » 2007-10-23 08:40:57

So permanent 1.1g would kill somebody?

#92 Re: Terraformation » Optimal human living conditions » 2007-10-23 02:40:02

Humor this hypothesis:

What if a human being's optimal living conditions are *not* terrestrial?

In that case, what would be our optimal living conditions?

Gravity: Is 1g optimal for humans? Wouldn't higher gs produce more stress and strain, and thus automatically produce a workout for everybody during the day? For example, 1.1 or 1.2g -- would an environment like that produce a "Bold and the Beautiful" civilization where everybody is in perfect physical shape? Wouldn't higher gs, with their musculature-enhancing effects, lower heart disease and other diseases of sedentary life? And if so, what would be the optimum? A 5g planet is probably too much, a 1g planet too little -- what might we humans want, for a good steady constant workout, but not to a damaging degree?

Pressure: Is 1bar optimal for humans? A lot of athletes train at higher altitudes in order to improve the oxygen processing rates of their blood. An athlete who acclimated to high altitudes can run faster, for longer, than their higher-pressure brethren. Might the optimal air pressure for humans be something other than 1bar? On the other hand, the athletes only receive their advantage when they come out of that low-pressure area into the high-pressure area. If the entire environment available is low-pressure, does that give any long-term benefits -- or even the opposite, does it damage us? Do high-altitude communities have lower scholastic performance or better?

Temperature: There's little arguing that 15-20C is pretty ideal for humans. But most environments on Earth receive a lot of fluctuation, both diurnal and seasonal. Would an environment that stays at a *constant* 15-20C (through whatever means) be better for humans, or are the fluctuations necessary to us?

Other aspects: (please add others)

Sum all of these together:

What is our optimal living planet?

#93 Re: Terraformation » Trojan Point Planets » 2007-10-22 18:50:36

A more precise but technical definition is that the Lagrangian points are the stationary solutions of the circular restricted three-body problem. For example, given two massive bodies in circular orbits around their common center of mass, there are five positions in space where a third body, of comparatively negligible mass, could be placed which would then maintain its position relative to the two massive bodies.

If the planets at trojan points were not of comparatively negligible mass, but on a par with the other planets, would the system still be stable?

#94 Re: Terraformation » Water Vapour instead of Nitrogen » 2007-10-21 22:23:00

So to put it concisely, if an area was pumped 100% full of water vapor and there was nothing else in the area, the gaseous H2O would automatically condense until only 35mmhg remained gaseous? No matter the ratios of H20/available volume? It would always gravitate, in any volume available, to 35mmhg of gas and the rest as water?

#95 Re: Terraformation » Water Vapour instead of Nitrogen » 2007-10-21 20:32:27

Austin, I'm not so sure it's "absolutely not possible". Perhaps you can clarify your statement.

What would happen if you had a hermetic dome, then brought in x tons of water ice, then used a vacuum pump to suck out nearly all the gases, then raised the temperature enough to melt the water ice? Wouldn't that produce an environment where the bulk of gas is water vapor?

For example, if the dome had 1Pa pressure from other gases (0.01millibar), the sublimation point of water ice would be (according to one phase diagram I found) approx. 220K. So heating the x tons of water ice to shirtsleeve temperature would produce x tons of water vapor as the predominant atmosphere of the dome.

Then, pump in some oxygen, and the original poster's question was, would it be feasible to breathe a mixture of say, 80% H20 and 20% O2? Or would we, I dunno, drown or something? Or would the two combine into H2O2 and bleach all our hair?

#96 Re: Planetary transportation » Given the recent rennaissance in Venutian Cloud Cities here » 2007-10-17 20:14:05

Mars will never be as good, simply because of its lower gravity.

If we ever develop technology on the level that you suggest (moving around dozens of bars of gases), Venus will be a paradise planet. Removing its extra gases will make it a much better planet than adding gases to Mars.

#97 Re: Planetary transportation » Given the recent rennaissance in Venutian Cloud Cities here » 2007-10-17 18:10:14

Because no other planet or moon in the solar system will be able to provide as close to earthlike conditions as Venus when terraformed.

And it will never be terraformed if we just stay out of it and ignore it.

#98 Re: Interplanetary transportation » Acceleration Gravity » 2007-10-15 10:02:56

Target values:

m = 100 000 kg
a = 0.00981 m/s/s (milligravity, one thousandth of a g)
t = 5 years (after halfway point, you have to start accelerating in the opposite direction so you won't overshoot your destination) = 158E6 seconds
v(peak) = a*t = 1.5E6 m/s = 0.5% of c (0.005c) velocity at the 5 year mark
E(peak) = 0.5mv^2 = 120E15 Joules expended to get to the halfway point
P = E/t = 759E6 W
v(average) = 0.5v(peak) = 774 000 m/s average speed for the whole trip
x(total) = v(average)*2t = 244E12 m ~ 1630 AU ~ 0.03 light years

So assuming 100% efficiencies all around (theoretical maximum) a 760MW power plant could accelerate a 100 ton ship at milligravity (1/1000g) for 10 years, getting 0.03 light years away in that time.

1/100g would require 76GW of power, would reach a peak of 0.05c at the five year mark, and would get 0.3 ly away.

1/10g would require 7.6TW of power, would reach a peak of 0.5c at the five year mark (relativity effects not included), and would get 2.6 ly away in those 10 years.

Unless we discover an antimatter mine in the inner solar system, TW ain't gonna happen. Even 76GW is unlikely.

760MW though, I could see as a space power plant one day.

#99 Re: Space Policy » Chinese Space Program? - What if they get there first » 2007-10-14 11:00:09

Well, I have a more optimistic view of the world than you evidently do. smile

#100 Re: Space Policy » Chinese Space Program? - What if they get there first » 2007-10-14 09:28:43

We're talking about preserving the fundamental rights of mankind, possibly for generations, and millions, if not billions of lives.

And you can preserve them perfectly well regardless of what the Chinese do. Their colonization efforts in no way weaken ours.

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