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I'd like to say that I did not see or read any previous discussion with avenger about private space colonization.
Just ignore it !
Most ideas come from other web pages, impossible to read all.
Some think they are important and all their ideas need to be remembered and credited.
Focus on concepts not on pecking order.
If you added Uranium and denser elements, sinking to the core, sufficient to increase gravity to that of Earth; the right mixture of radioactive materials could heat the whole planet to a comfortable temperature.
Where to get very dense and radioactive elements ?
We might get lucky and find the remnants of a supernova, somewhere in the Oort cloud, drifting in from interstellar space. Even the Sun is thought to have an Iron core.
It sound like you still need some type of small chem based rocket to push to orbit. Just enough thrust to over come drag, and carry fuel
Could try beamed power.
But then, there is the Sun already, just need to focus the light onto a small cylinder,
using hydrogen as the propellant.
Using beamed microwave for Exhaust of 8 km/sec:
http://monolith.caltech.edu/Papers/ParkinThruster.pdf
http://monolith.caltech.edu/Papers/ParkinLauncher.pdf
$ 20,000,000,000,000,000,000 = 20 Million Trillion Dollars ?
Borrow it from the Chinese govenment ?
The effort to make Mars a greenhouse, swamps of Florida, wiithout a roof ?
Add more mass to Mars, solar reflectors etc.
The sky is the limit, may be impossible in this century, at any cost.
Roof and insulate well, that we may be able to afford.
The technology needed is self replicating robots.
Lot of solar cell generated power to build comfortable accommodations for the settlers.
Safety first, using the best technology will prove quickest.
If you had asteroids in momentum transfer orbits between Jupiter and Saturn.
Eventually the 2 orbits could be made the same; Orbital energy and momentum conserved. Hence the heat energy in colliding Saturn and Jupiter is only the gravitational plus rotational interactions as they become one planet.
Calculate combined orbit radius from energy conservation.
Other extreme is head to head collision. Make Saturn retrograde orbit.
Lot more heat, merged orbit closer to the Sun. Orbital energy not conserved.
M1 * V1 + M2 * (V2) = (M1+M2) * Vf In circular opposite direction orbit V2 = -V1
1/2 * (M1+M2) * Vf^2 is remaining energy in motion.
Calculate orbit radius from energy remaining.
GMm/r - how to calculate the effective r ?
If it were incompressible fluid then assume a shell above Jupiter surface,
mass of shell converged to one point at a distance r from Jupiter's center.
If compressible gas shell and solid core, then seperate calculation for each.
http://www-formal.stanford.edu/jmc/futu … node3.html
From there, calculate rise in temperature from specific heats.
I see it as an issue of expanding in an expedient, cost effective way.
Near Earth first because it is quick and various projects overlap.
Time is money. Control from the Moon enables other projects.
"with the Russians claiming that the answer to all our energy problems is tied to having bases on the moon, it’s clear that the big sell for the next space race has begun."
build a spacestation up in orbit that has heat shield reentry capsules
The idea has merit, just dock into a re entry station, like a subway transfer station.
Maybe even decelerate into an evacuated ramp from space to Earth.
Instead of a heat shield, use a linear motor to brake.
I thought of sneaking in a few Hydrogen composition objects in place of the water based ones. Don't kmow if can make a giant Hydrogen bomb that way.
After the first few have made a deep hole, a properly placed bomb inside the mantle, with other masses behind could really blow things up.
They seem really confident that they can get a lot more for their yen then NASA gets for their buck
Smart Japanese become Engineers.
Smart in USA become Lawyers, needed to control the Global Empire.
US uses Foot Slug System while Japan uses the Meter Kilogram System.
Slugs got US to the Moon at high expense but the future is lower cost Metric.
Better cars from Japan, soon better rockets also.
Moon sooner and takes less time than asteroids.
Part of near Earth infrastructure of cyclers and
electric launch of products from Moon factories.
The supply line to asteroids is too long.
Do we need hundreds of iron asteroids or just 1 or 2 traveling at very high kms.?
Mars plus Sun escape is only 39 km/sec,
Optimistic gravity assists from gas giant planets might give 50 km/sec total.
Cannot think of a way to get more from within the solar system.
Substitute liquid hydrogen in place of icy objects and try for thermonuclear ??
need 1 Giga Kelvin at least http://en.wikipedia.org/wiki/Nuclear_fusion
from: http://mooni.fccj.org/~ethall/gases/gases.htm
u^2 = 3RT/M T=u^2 M /3R R=8.31
50,000^2 * 2 / 3 * 8.31 = 200,561,572 °K is only 20% required temperature.
If you has 2 objects colliding at 50 km/sec fot a total of 100 km or 802,246,289 °K
Not enough, so need fusion as a starter in a hydrogen bomb.
But some velocities are considerably greater
http://csep10.phys.utk.edu/astr162/lect … press.html
I think it is almost one and a same thing whether single ball of 100 km ice impacts Mars, or shower of "shrapnelled" into millions of chunks 100 km ice ball ... The showering creates better areal distribution...
Going extreme other way:
Line up 100 of these Oort cloud objucts, aim directly towards Mars's iron core.
If they hit one right after the other can the iron core be reached ?
Extreme high density and termperature plasma, similar to ati tank armor piercing.
Average temperarure rise of Mars almost 1,000 K.
Lot of vulcanoes and 2.8 meter water after cooling down.
Sorry, Made mistake
Cubic meter water weighs 1,000 kg not 1 kg
So temperature raised 1,000 times more, by 9.7 °K ?
Will recheck water level also
==========================
2.88 cm seems correct = 1/3 (100^3 / 3397^2)
Volume = 4/3 pr^3
Surface = 4pr^2
==========================
Impact deep and vaporize some of Mars to escape velocity ?
some Delta V numbers:
http://fti.neep.wisc.edu/neep533/FALL2001/lecture28.pdf
Perhaps can get close to 50 km/sec on Mars impact from Oort cloud.
Mars Surface escape + Sun escape + Jupiter gravity flyby.
Assume 100 km diameter water object specific gravity = 1
1/2 m v^2 = 1/2 (4/3) Pi (10^5)^3 50,000^2 =
2/3 pi 10^15 25 10^8 = 52.36 10^23 joules
Mars Mass: 6.421 X 10^23 KG
Basalt rock 0.84 10^3 J/kg °K
(52.36 10^23 joules) / (6.421 X 10^23 KG) = 8.15 joules/kg of Mars
8.15 / 0.84 10^3 = 9.70 10^-3 °K = 0.0097 °K almost one hundreth of a degree
Need lot more to melt Mars
Average depth of water:
4.19 10^6 km^3 / 1.448×10^8 km^2 = 0.0282 meters of water
Mars — Diameter: 6,794 KM for fun, plug numbers here:
http://www.stardestroyer.net/Empire/Sci … roids.html
will recheck this
Ice is a solid because of hydrogen bonding between molecules, while rock is a solid because of ionic (or sometimes covalent) bonding. Hydrogen bonds are relativly weak, and Ice would creep over much shorter time scales.
Strength of hydrogen bond increases with pressure, according to expert opinions.
You realize a lower viscosity works against you as viscosity is the tendency to resist flow
True, can guess at strain rate.
10^-15 would be considered a solid = 30 million years.
Extrapolating one graph gives around 50° K for that figure.
Have not found any measured data for low temperatures at 1 TPa.
However such high pressure exists only at the bottom center,
reducing strength requirements.
Worst case is angle of repose, 1.5 to 1 slope giving 300 km base.
Will calculate energy to freeze, cool the ice, and keep it cold after.
Ice is a solid because of hydrogen bonding between molecules, while rock is a solid because of ionic (or sometimes covalent) bonding. Hydrogen bonds are relativly weak, and Ice would creep over much shorter time scales.
The properties of high pressure, low temperature ice are not well known.
100 km is around 10,000 atmospheres; for 2,000 atmospheres:
"These new results show that the viscosity of a deep icy mantle is much lower than we previously thought," said William Durham, a geophysicist in Livermore's Energy and Environment Directorate."
http://www.sciencemag.org/cgi/data/311/5765/1267/DC1/1
Viscosity = (shear strain rate)(Stress)
http://www.uwsp.edu/geo/faculty/heffera … nrate.html
Base might approach 10^12 Pa or 1 TPa
Not quite metallic water: "The calculated pressure of metallization 1.76 TPa"
The recent data might prove you right. Will have to plot and see.
But extrapolating this way is just guessing.
But anyway, this idea is sheer lunacy, to build a mountain range 100km+ high and 800km long right at the equator would surely take more energy then the Earth has to offer for the project. I won't even bother to address this idea any more, its insane.
Volume of water possibly same as Greenland glaciers.
Will calculate the number for solar days or years for the area covered.
====================
Calculate parabola from here:
http://epsc.wustl.edu/~epsc353/lectures/flow_03_p1.pdf
1) freeze such an amount of water;
2) keep it frozen.
water latent heat of fusion = 334 (kJ/kg)
Heat capacity (solid 0 °C) = 2.06 kJ/(kg·K)
Water freezes at higher elevations, but need energy to lift it there.
Insulate top with styrafoam/aereogel combination ?
Bottom, just absorb the geothermal, as Antarctic ice does.
Will plug in numbers later.
Oh, and how are you supposed to keep the BASE solid? at that kind of (weight-induced) pressures?
Hint: liquid H2O is more compact than Solid H20...
"The minimum temperature that liquid water can exist without ever freezing is -21.985°C at 209.9 MPa; at higher pressures water freezes to ice-three, ice-five, ice-six or ice-seven at increasing temperatures"
taken from: http://www.lsbu.ac.uk/water/explan2.html#Pmelt
Talk about a dead in the water kind of idea...
Greenland is melting. Hide the extra water where ?
Solar energy is greater in the tropics, easier to do than cool Greenland.
===================================
If you build a tower out of ice, reguardless if the ice can support the weight or not without outright fracturing, it will squish like a marshmellow in a frying pan.
Function of temperature; the question is over what time frame ?
Bedrock creeps over geologic time.
Trying to learn the answer.
Did a plot at bottom of page for area per 100 meter changes in depth:
http://www.geocities.com/marscatdog/
There is a peak at 4,200 meters, hitting large areas of ocean bottom.
Summing area times each depth is numerically integrating, to give volume.
You gain a lot of land first 100 meters, 22,100,000 km^2 or 4.3% imcrease in land area,
then only 1/4 as more the next 100 meters.
==========================================
The page takes too long to load
will reduce some of the diagrams later.
I changed the program to calculate WGS 84 ellipsoid,
but little difference from simpler spherical model.
Interesting that some experts want to abandon the WGS 84 altogether.
HOw does it trades between timing and cost ( energy budget)?
Simpler, direct transfers, can calculate time,
but complicated slingshot encounters and a lot of possibilities.
When things are lined up, Iapetus slingshot towards Titan could give a boost.
Closest approach at sum of their radius.
For example, theoretically, you could destabilze an collide the whole solar system
with slingshot momentum transfers. Take an asteroid, do momentum transfers with other bodies, untill the whole solar system collides into itself.
Earth's orbit diameter has resonance with Jupiter, which is stable.
But what would it take to have Earth ejected from the Solar system ?
Sun is pushing away the interstellar gas.
So we are stuck with with only materials as far as the Oort cloud.
" It is believed that the total mass of comets in the Oort cloud is many times
that of Earth, and estimates range between five and 100 Earth masses."
Maybe there is a water planet there, just the right size, ready to be moved.
Eventually, mining, disassembling the gas giants seem plausible, but
will have to look up how.
===================
Back to andrew's supposition:
Martian rocks have been dated to be cold for very long time.
Impact would have warmed Mars.
Dating of surface and interior profiling of Mars might produce something suprising
A mountain range of ice 800m long, 100km high, and probobly at least 100km wide?
For simplicity assume equilateral triangle, rising from sea level.
2/sqrt(3) * 100 = 115 km base at sea level.
Appoximate form for ice fields is a parabola. Very shallow near melting.
How low temperature for what size base ?
Trying to find out.
You are out of your mind,
thats bigger then most of the equitorial countries that could host the thing.
Countries in drought could use an ice mountain ramp range, even if well insulated.
Think of the precipitation and rivers that would flow from it.
Space tourism, downhill skiing ? put on your spacesuit first.
Only 8 meter drop in sea levels, so New Orleans would need smaller dykes.
If you built 12 of these then Earth would gain extra 4% land area.
No material made by man could build such a structure, it would collapse from its own weight. This thing will be 100,000m/340,000ft high!
"The best graphite epoxies I know of (Amoco 'Thornel' type T40 carbon fiber + type
1962 epoxy) have a compressive strength of 250,000 psi and a density of
0.06 lb/cubic inch. Thus their scale height is 4.16 million inches (106 km)"
For 1 billion dollars 111 mile high tower is given:
http://yarchive.net/space/exotic/tower_launch.html
http://campus.murraystate.edu/academic/ … carthy.pdf
==============================
see for scale height equation and explanation:
(bottom area is 2.718 times area of top for the scale height)
http://en.wikibooks.org/wiki/Space_Tran … /Methods/1
Amoco T300/ERL1906: 1930 MPa / (1827 kg/m^3 x 9.80665 m/s^2) = 107,793 meters
steel: 125 MPa / (7800 kg/m^3 x 9.80665 m/s^2) = 1,635 meters
Ice: 20 MPa / ( 920 kg/m^3 x 9.80665 m/s^2) = 2,218 meters
So scale height for Ice is comparable to steel
Advantage of ice is that it floats, while steel sinks towards Earth's center.
==============================
Looks like 2 ways to build ramp to space:
(1) use very high strength materials for slender 20:1 base/height structure
(2) Giant low slope ice ramp
Force = G * M / r^2 is same for water world
M = density * (4/3) * pi * r^3
Substituting: F = G * demsity * (4/3) *pi * r^3 / r^2
Equating Earth and Water World, cancelling to get
density1*r1 = density2*r2
5.5 times Earth radius
You are correct
Total volume is 166 times Earth and Mass is 30 times Earth.
Escape velocity
11.2 * sqrt(30/5.5) = 26.2 km/sec
Then the atmosphere interactions ?
numbers from here:
http://www.enchantedlearning.com/subjec … oons.shtml
Plugging here:
http://home.att.net/~ntdoug/smplhmn.html
5437.185110416846 - 1706.704095229685 = 3730.481015187161 m/sec
"Low-thrust transfer
It can be derived that going from one circular orbit to another by gradually changing the radius costs a delta-v of simply the absolute value of the difference between the two speeds"
Slingshot off Iapetus would give lower number.
Giant ramp to the sky... evacuated tunnel 100's km long... maglev track up to Mach-20... still only able to send up one at a time... massive destruction from a "derailing."
Evacuated tube on top of the ramp. Should be safer than normal maglev because all in straight line. Think of it as a giant sized particle accelerator.
The orbital velocity at 100 km is 7.85 km/sec
At 4G acceleration:
V^2=2*4*9.8*d d = (7850^2)/(8*9.8 ) = 786 km
time = sqrt(d/(2*9.8 )) = sqrt(d/(2*4*9.8 )) = 100 seconds
Cargo can stand higher G and be accelerated to Earth escape of 11.2 km/sec.
Then there is the ungodly amount of energy needed to make this ramp of ice, and to keep it from melting. How many trees would have to be cut down to make a "wedge" of ice 100's of kilometers long and 100km high? Answer: all of them
Ok, will calculate energy needed in a day or 2. Several miles up, water freezes by itself, so just need to lift it and cool it further to 150º K. Insulate with a meter of styrafoam - will calculate guessed heat loss. Wood chips were used to make the ice ships less brittle, might be an alternative to burning sawdust, hide it inside the ice and gain Kyoto CO2 credits.
And it still wouldn't even support its own weight, the pressure would make the foundation deform and squish like a marshmellow being run over by a tank.
In the North, permafrost supports. Heavy trucks cross lakes on floating ice roads.
http://www.mvp-wc.usace.army.mil/ice/ice_load.html
From: http://www.nationalgeographic.org/seala … eek_3.html
" The catch is that because frozen sea ice has roughly the strength and resistance of a block of concrete"
Considerably better than regular concrete (20 MPa) is 150º Kelvin ice (60 MPa).
http://www.geokhi.ru/~planetology/these … ov_b_a.pdf
"The most common use of high-strength concrete is for construction of high-rise buildings. At 969 ft (295 m), Chicago's 311 South Wacker Drive uses concrete with compressive strengths up to 12,000 psi (41 MPa) and is the tallest concrete building in the United States."
Ice is still brittle near freezing point,
as evidenced by giant cliffs when a glacier breaks up into the ocean.
http://images.google.com/imgres?imgurl= … 26sa%3DN
Idea is to build a large ice ramp along the equator,
starting at Pacific Ocean sea level, slowly rising to 100 km.
Evacuated tube with linear motor for propulsion.
Ice is considerably stronger when cooled, maybe 10 times at 150 Kelvin.
Ice ships were almost used in the second world war
http://www.google.com/search?client=ope … 8&oe=utf-8
As a bonus, if you build a big enough ramp,
lower ocean levels, and New Orleans is saved !
Billions for dykes or ice ramp to space ?
The asteroids and small moons will be valuable as momentum transfer objects.
So preferred would be moving large Moons and Kuiper objects.
I like the idea of mutually tidally locked planets in Mars orbit.
Make a large water planet of 1G, floating cities etc.
They could be even be so close as to share a space elevator at the center of gravity.