Integrating all the best ideas for a much needed space race of private sector enthusiasts… Mother Earth calling – “She’s buying a stairway to heaven”

Image result for space elevatorWelcome to the team of future thinkers, investors, and yes, astronauts (we can all go to space, one day we must!), a think tank designed to create the first space elevator (SE), deploy satellites, people, and cargo into space, what will soon be a multi-trillion dollar industry, and eliminate expensive, dangerous launches.  We must be able to have infrastructure providing lift to orbit… not expendable (even reusable does not close the equation) launches. We are open to all kinds of ideas and my idea does fall into a great solution, as the cable designed to support an elevator well beyond geosynchronous orbit, or GEO (where a space station [SS] is always in the same position relative to a fixed observer on earth) was something thought to be impossible because under gravitational pull from earth on cable, fighting equal and opposite centrifugal force (the inertial reaction, or resistance to acceleration, to the centripetal force pulling you toward the center of the earth, like when you drive your car around a corner and your body goes outward) will snap, even with the toughest of high tensile strength, low weight (density) material, like carbon nanotubes (CNT) are used. But now we’re back, as my computer modeling, employing the idea of a hollow tube or Space Hose (SH), also called the Space Elevator and Coaxial Cable with Internal Material Transportation, or SEaCCIMT for short, instead of a solid cylinder or ribbon, much lighter, the advantage of a cylinder but high-leverage ribbon (when it’s compressed and elliptical) will allow semi-permanent flow inside hose of hydrogen and oxygen to power counterweight (CW) base-station at end of hose(s) with rockets to eject propellant away from earth to prevent hose from snapping, making sure it always has a little slack, never too tight or taunt. The hose would have to extend overall to at least 60,000 miles in altitude for the CW at the end (unless hose thickens in outward direction. It would have to extend further with increasing diameter/thickness without a heavy “bulb” at the very end) to create centrifugal forces contrasting gravity, or else the assembly crashes back to earth. The initial first of three x 60,000-mile hoses is extended in different segments after numerous rocket missions where GEO SS is constructed first, both outward from the SS at GEO, and inward toward the Earth Starting Station (ESS), as rocket launches are only required for the first hose of 60,000 miles. So a 3D CNT Printinghexagonal-sided elevator is stable once two additional SH’s are dragged by first elevator upward, when only one hose is required in the beginning and the other hoses don’t require rocket launches. One hose supplies the CW rockets with oxygen, the other two hydrogen, as rocket fuel requires the 2:1 ratio of H2 to O2 for maximum (loudest) burning efficiency, and conveniently starts that way as water (H2O) at the equator of the Pacific oceans where electrolysis converts it into separate gases. An SH can eject rocket propellant inward, outward, or north, south, east, and west, while hose extensions are added, and then half the day in the lifespan of the SH assembly outward during the two apogee phases of an elliptical orbit where the CW experiences a greater force outward. The other 12 hours, H2 and O2 can be stored for the next apogee fuel ejections, or other purposes.

CNT alone as a cylinder will break at 1 meter, correctly pointed out by a study by GoogleX, as gravity versus centrifugal force is too great for a cable where center of mass (COM) is at GEO, or 35,786 km (22,236 mi). The total gravitational field on all points when the cable is tight is:

g = – G x M/r^2 + ω^2 x r

g is the acceleration of apparent gravity, pointing down (negative) or up (positive) along the vertical cable (m s−2),

a is the centrifugal acceleration, pointing up (positive) along the vertical cable (m s−2),

G is the gravitational constant (m3 s−2 kg−1)

M is the mass of the Earth (kg)

r is the distance from that point to Earth’s center (m),

ω is Earth’s rotation speed (radian/s).

At some point up the cable, the two terms (downward gravity and upward centrifugal force) are equal and opposite. Objects fixed to the cable at that point put no weight on the cable. This altitude (r1) depends on the mass of the planet and its rotation rate. Setting actual gravity equal to centrifugal acceleration gives:

r 1 = ( G ⋅ M / ω ^ 2 ) ^ 1 / 3

See https://en.wikipedia.org/wiki/Space_elevator.

Image result for carbon nanotubes
Carbon nanotubes (CNT), which can be extruded into a small, thin-walled hose.
A small capsule, either launched from earth with SH tethered below, or assembled in space to drop SH in sections, will expel rocket propellant in 6 directions to maintain “slack” and prevent SH from breaking.
3D Injection Molding Printer can produce a 2 cm hose quickly, when fed, in little time with little human participation, polymerized CNT. 1,000 square foot homes manufactured this way only cost about $4,000.

A polymer / CNT – reinforced hose will transmit H2 and O2 through the inner cavity after electrolysis to strip two-parts hydrogen for every one part oxygen, for maximum rocket “loudness” and efficiency, separated by a viscous oil or “moving gasket”, so the ESS will use gasoline/charcoal generators to convert sea water, available in high abundance at an equatorial Pacific island or boat, with solar panels/wind turbine as backup. The moving gasket will allow a liquid diet, nitrogen, and other substances to be transported. The hose can be effectively, quickly, and inexpensively be manufactured with a 3D injection molder printer, see http://www.mdpi.com/2079-6439/5/4/40/pdf. On the other hand, you can have 3 hoses for 3 rocket-injectors, 2 H2 and 1 O2,  that eject H2/O2 propellant 10-50% of the time, mostly away from the earth, sometimes in any of 5 other perpendicular directions. “Tension” sensors, backed up by a computer that controls timed and spontaneous fuel ejections for more burnt fuel outward when there is more tension, will be necessary, with a reserve and 24/7 human surveillance. An additional set of 2 hoses can extend to a total of 60,000 miles from earth for a highly eccentric (long, flat elliptical path, or high aspect ratio) orbit, so space crafts/artificial satellites benefit from the high tangential velocity of the hose-system alone, even without fuel, and can easily be slung into an orbit to approach Jupiter and use a slingshot effect from its intense gravitational pull to go deeper and faster into outer space, well beyond Pluto. The goal, more than anything, is to prevent

Highly exaggerated elliptical orbit of CW around earth (high eccentricity, larger aspect ratio of semi-major axis versus semi-minor axis), where center of mass of the Earth is at one of two foci. Energy must be sufficient to pull CW in hundreds of miles twice a day when approaching apogee to prevent breaking. However, a highly eccentric orbit is considered to be a good thing, as: 1. The higher speed when approaching the lesser of two semi-major axis means a sling-shot effect, for hurling satellites and space crafts deep into space without the need for much, if any, rocket fuel, and 2. While energy is always conserved regardless, when it comes to accelerating Ferris Wheels pulling CW inward and the less common situations where rocket fuel at end of hose is needed for ejections, the Ferris Wheels must decelerate anyway after accelerating, which is reverse acceleration and the counterweight is pushed outward, but over a long enough period of time when approaching and leaving the semi-minor axis, that is tolerable because their will be plenty of slack in the hose

cable/hose from snapping, keeping it in a permanent bent-shape and never too taunt. The role of the 6 rockets at CW is to keep the elliptical orbit of the CW as circular as possible, or have the lowest possible eccentricity, so that a predefined minimum bend in the hose can be defined as the aspect ratio of the length of hose (60,000 miles) versus deflection from straight position, say, 500 miles, a catenary shape, which pulls the CW inward about 200 miles. 200 miles is an arbitrary “comfort zone” for a radial-direction shortening of the semi-major axis to a point less than average radius. A semi-stationary cable, by fiat, expects to have a very high orbital eccentricity such that preventing atmospheric re-entry becomes difficult at GEO, with Coriolis forces considered. But repositioning rockets, and that means lateral directions as well, can retain the desired position. In conclusion, the energy expended during two 6 hour apogee phases by the CW rockets, and/or energy from torque of “Ferris Wheels” (see below) must exceed the energy of the SH centrifugal force, with increasing help from the gravity of the SH as the CW moves inward, and then must slow down, to prevent the shearing of 1-2 cm diameter hose, and causing the CW to crash back to Earth, finding an equilibrium point that may require 24/7 “eccentricity adjustment” for the most circular orbit possible. A thickening of the SH at GEO might be recommended even if free breaking length might occur elsewhere, and future calculations prove just rocket fuel and Ferris Wheels, even as backup, are not an exclusive and legitimate insurance policy. More elasticity can help, something to be expected with a higher diameter, thin-walled hose, with a higher ratio of HDPE to CNT. The true requirement of hose rocket fuel and torque created by Ferris Wheel counterweights is that it must exceed the breaking force of the hose at it’s weakest part, the center of mass at GEO, with a gradual reduction in thickness and resistance to breaking in opposing directions. The thickening at COM does not effect the gravity plus centrifugal force high tension threat, unlike when more weight is far from the COM, but the increased number of rocket launches would probably be un-affordable unlike when you have a “kill many birds with one stone” option. A well-made non-hollow cable could employ Ferris Wheels without the need for material transfer, but there is the danger of no-backup. The best way to come up with a computation is:

SEaCCIMT AnimationCatenary

This implies a solid cable, CNT-HDPE, will have to be 25,000 times as thick as the presumed 1 cm diameter it starts with, or 250 meters, tapering off gradually in both directions. This is highly unrealistic and would require tens of thousands of rocket launches for something, under the stress, strain, and wear of the most valuable part of the cable, the “weakest link”, and would make a 0.5 trillion-dollar boondoggle the most reckless gamble in world history. If the cable were more dense but not that much wider, say, if you go from 5% CNT at ESS and CW to 95% CNT to COM, you can reduce physical diameter 19 times to about 13 meters, but the serious reduction, on average, in tensile strength divided by density means far too many rocket launches, and the space hose, no matter what you do, will save on the true expense, 99% on rocket launches alone. Also, an elevator travelling to and from something 13 meters in diameter will move much too slow for acceptance. There will soon be a way to guarantee the entire hose will be 90-95% CNT anyway with 3D printers, with the much needed backup of rocket fuel to assist Ferris Wheels, and a constant supply of oxygen and water as permanent space colonization, from my standpoint, will not risk anything life saving. The hose would have a much longer free breaking length than the solid un-tapered cylindrical cable, but all that is needed is something that allows CW rocket fuel and the torque of Ferris Wheels to overcome a small percentage of the combined total gravitational and centrifugal forces.

In addition, 24/7 H2 and O2 not only for rocket-propelled slack of SH, but for fueling/refueling space crafts, oxygen and water for astronauts for long term space residency that cannot be easily recycled, as well as food capillaries, nitrogen (N2) for higher-temperature liquid freezing necessities, etc. Thinner hoses that are less likely to support liquid/solid transport are lighter and easier to launch, and can transfer H2, O2, and N2 only, with hydrogen and oxygen recombined for water at SS, and rocket fuel at the CW, for what now should be called the Hose Stabilizer (HS). Liquid and solid add weight and tension to the cable, and even though rockets will always be there for correction to too much tension, it is best not to over-challenge it. Food can otherwise be transferred by elevator, grown on a space farm easily with intense radiation and recycled carbon dioxide, with fruits/vegetables, stem-cell meat, etc.

The elevator that moves up and down the SH can compress it and move along it with rollers driven by three gasoline engines in one direction. Hypothetically, if some liquid were allowed, with hydraulic pressure pushing elevator upward with high pressure below it, suction on liquid and gas the in tube above also adding to upward momentum. A magnetic field from superconducting magnetic that has affinity for H+ atoms in inner hose (top) and repulsion from OH- molecules in inner hose (bottom), for extra lift on top of roller engines, can also increase velocity, for partial electrolysis initiated at ESS. A liquid nitrogen cooled superconducting magnet can even respond to the conduction of electricity through the CNT core of hose (carbon is highly conductive), causing speeds up to hundreds of miles an hour. With the benefit of the pinching of the motor’s rollers on the SH, causing an ellipsoidal “ribbon” effect, for a better grip, the ability to get crew/robots and cargo to GEO can occur in one to five days.

Space Hose Horizontal Cross Section 2
R = 1 cm, r = 0.95 cm, with no need for increasing diameter outward to create counterweight effect, as launch of heavy “bulb” or Ferris Wheels to become the very CW 60,000 miles away, causing inward push from torque is necessary backup. CNT-HDPE wall thickness is at least 0.5-1.0 mm. The “pinching” effect of rollers from the elevator give hose elliptical ribbon shape, giving elevator more leverage, with need for rollers only in one direction. Repairs on tubes that may puncture with loss of very small H2 molecules are easily done when you have 2 backup hoses, as one must consider wear, stress, and strain from elevator rollers and meteorites. But with a constant slack in the hose, the elasticity and therefore durability of the hose from meteorite strikes is greater. As the diameter goes up with a fixed wall thickness, the weight, per unit length, goes up by  Π x (R^2 – r^2) x Length, so a bigger diameter hose, with a bigger inner diameter for more fuel transport , goes up in fuel weight by r^2, increasing at more of a rate than R^2 – r^2 (R – r = constant), so the average density of the SH becomes less, with more of a pinched gripping effect for rollers, and more elastic. A bigger hose may be worth the extra number of rocket launches




Space Hose Along Axs with ConnectorKevlar was once considered as a cheaper, more readily available exclusive substitute for CNT, with more elasticity, but because conventional Kevlar has about 1/18 the tensile strength/density ratio of CNT (3.62 GPa vs. 62 GPa), it would be impractical as a non-hose cable, because of the extra weight required to overcome breaking length limitations. The proposed new polymer substitute is high-density polyethylene (HDPE) which is non-H2 permeable. Both have about the same density, 1.6 g/cm^3 for CNT, 1.44 g/cm^3 for Kevlar/HDPE. The break would most likely occur in the middle, which can be thicker, but would require 2.4 to 2,441-times more dense a cross-sectional region, based on the “free breaking length” which is the length the equivalent solid cylinder that would break under it’s own gravity, even with a breaking length at 1/10 the total distance, yielding the 2,441 figure. Software modeling/simulations cannot develop a solid cable concept, low-weight and affordable enough, where you can assure safety from too-many possible bottle-necks. The increase in the size of hose, which need not be 2,441 more dense thanks to fuel emission outward during near-apogee, can slowly become smaller out toward the CW orbit. In addition to the threat of a longer hose assembly breaking because of a potential delay of H2 and O2, solar-powered “Ferris Wheels” (see below) will provide some of the necessary backup. The CW can be a second space station, like the one at GEO. Multi-threading was another proposal, well beyond the three I proposed, but too many threads if solid cylinders are required for a reasonably small elevator presenting great expense, time delays, and most importantly, you’re just increasing the weight-centrifugal force opposition by the factor of the same additional threads. Three times the number of rocket payloads, with the first hose/cable necessary for one of three of six sides of the elevator (skip each corner of hexagon), are unnecessary as the additional two hose/cables can be dragged from the earth base-station that can thread the additional two “corners” of the hexagonal outer-elevator and guarantee longer hose/cable-complex lifespan, most importantly, it means maximum safety. Unless the hose thickens outward to capitalize on centrifugal force, there will be a need for a large counterweight (CW) that must be launched as usable dead weight at the end, 60,000 miles away from earth), with elevator missions as the best option for dragging additional cables, even if CW has not be created, as rocket fuel can eject emissions as backup, toward earth at GEO until more elevator missions extend cable outward from GEO, and then inward toward Earth to complete third segment, until CW-effect is completed, eliminating more rocket launches. It’s predecessor can be mass-produced as wireless coaxial cables for cable TV/Internet are now ramping up in China (and we can consolidate industries because much needed satellites for thousands of applications will use cable as back-up, but fear of the “dark angel” threat makes satellites that much more necessary and profitable. But the miracle of CNT for many applications, like football helmets, strong and lightweight means you don’t have to sacrifice head injuries for neck injuries, and vice versa, engines and other parts for cars, $4,000 1,000 square foot houses, etc., made possible with 3D printers, we can capitalize with our weighted-average industrial democracy corporation (IDC) in the making for instant cash-flow even before the SH and elevators deploy with the many profitable satellite missions that bring in possibly the highest return-on-investment ever!

Space Hose cross section
Polymer/Kevlar hose, reinforced, or impregnated with 100 nm CNT tubing. Walls can be as little as 0.5 mm thick, and non-gas-permeable, for total diameter of preferably 3 mm but very low total density for low weight, high inner-diameter for maximum flow of matter, and low number of launches to complete section up to GEO. CNT in it’s natural state is a cylinder, with 100 nm diameter fibers extremely strong, but could be grown in HDPE with inner diameter any size desired.

For a 2 cm diameter polymer/CNT-reinforced hose, with 1.8 cm inner diameter hollow region, hence, 1.0 mm (about the length of an ant) non-gas-permeable polymer, the following calculations are used to show the SH can be light enough for under 3,000 launches/payloads for the 180,000 miles of hosing, to get started, SS construction as well. The hose will hypothetically be 90% CNT, 10% HDPE for now, which leads to the following calculations:

Density = 1.6 g/cm ^ 3,
Density = 1.44 g/cm^3;
=> Avg. Density = 1.56 g/cm^3;

1 cm = 10 mm,
1 cm ^ 3 = 1,000 mm^3,

0.00156 g/mm^3 x {(3.1415 x [10 mm]^2) – (3.1415 x [9 mm]^2} = 0.09311 g/mm = 93.11 g/m = 93.11 kg/km;
1.609 km/mile x 2.205 lb/kg x 93.11 kg/km = 330.3 lb/mile;

60,000 miles x 330.3 lb/mile = 19.82 million pounds = 43.70 million kg = 43,700 metric tons;

That figure can be dropped to 1/4 the total mass if SH wall, after thorough testing for H2 permeability, stress, strain, and shearing factors, can be manufactured at 0.5 mm in thickness, and less if diameter is reduced to 1 cm. Dragging missions can also be cut to a forth of the work if safety/feasibility testing shows the same smaller/lighter hoses can be used.

Space elevator
Space elevator, rolling upward/downward with motorized rollers, when going up, suction on top, pressure from bottom, for extra hydraulic push/pull, and magnetic field with affinity for H+ atoms on top, repelling OH- atoms on bottom, suspended in semi-aqueous/vapor solutions. This will reduce roller-induced fatigue on hose and be more energy efficient, less gasoline needed for long trips, with intense cosmic sun rays, above 130 km, producing enough electricity for freezing N2 for super-conductor. This diagram is exaggerated for what should be six-sides, not four, and absence of liquid H2 and O2, gas only, with the superconductor moving because of CNT electricity conduction may better serve the purpose of moving elevators at high speeds, magnetically levitated for the same speeds as high speed trains

The Falcon Heavy rocket, with reusable side boosters, costs $90 million. For a fully expendable variant of the rocket, which can lift a theoretical maximum of 64 tons to low-Earth orbit, or 58 metric tons, the price is $150 million. While it is not certified yet, SpaceX says its rocket can hit all Department of Defense reference orbits; however big and gnarly the military wants to build its satellites, and whatever crazy orbit it wants to put them into, the Falcon Heavy can do it. This means about 750 trips to engage first into GEO to unfurl the first spool of 60,000 miles of 2 cm diameter/1 mm thick-wall of hose/cable, 180 for 1 cm diameter/0.5 mm thick-wall, not counting missions to build SS, CW, and of course ES with multiple elevators. and cost of fabricating 180,000 miles of hosing. The minimum total cost would be $30 billion, and not more than $120 billion, so only if my 12/7 H2/O2 GPS-corrected rocket propellant position correction idea flies with the joint venture capitalists (JVC’s), which is all of you, we will spend far less than a proposed CNT-space contingency, Obayashi, who are willing to spend $500 billion without a doable model, proposed to be built by 2050, even after GoogleX dashed others’ hopes in 2012 with the 1-meter breakage study for a single high tensile-strength, low density CNT-only solid cable. I am not a metallurgist or chemist, a physicist mind you, but while breaking length is now negligible because of my proposed permanent slack in hose/cable, the decreased expense in a hollow cable might be offset by the production cost of extruding CNT with a hollow center. If the industry is doing well because of the “you win, I win” benefits of the CNT for other things, they can be mass-produced in a tax-diminishing society cheaper and terrestrial applications can fund our efforts, the way we’re trying to do it with donations, where there will be a raffle for donors to be considered as space tourists (see Donate/lottery), products, etc., and I will add to it a foreign business license with stock options, instant profit sharing (see Become a Member and Profit!, job opportunities as well) with “industry merging” and all online revenue collections, lotteries, charging memberships (we can be affiliates to each other, the way I am encouraging people to promote the URL “SpaceHose.com” with your own creative logo, with your own memorabilia) and be rewarded affiliate commission, online gaming, sell CPC/CPM advertising on Web pages, video, or even in space, etc., many great ideas, but the key is paying for advertising, especially as a start-up. I can probably get Facebook advertising, the charge as little as 0.0003 cents/impression, if I pool together many investors. My other advertising websites “integration of the best ideas” – https://www.PandaBusters.com (available now, multi-tier affiliate programs with high search engine rankings), https://www.InvestorCommune.com, and https://www.MyRatingSearch.com (under construction) will allow us to promote this portal and yours to sell what we all want to sell and raise capital for a much needed space race.

Space Hose stretchingAs back-up for the possibility of the loss of rocket fuel to guarantee slack in hose, and “killing two birds with one stone” because of the need for a heavy CW at the 60,000 mile end of elevator shaft, the CW, with enough mass and large enough radius because of a series of “Ferris Wheels”, torque (T = M x A x R, where M = Mass, A = radial acceleration, and R = radius), causes the CW to move inward, perpendicular to direction of rotation. If enough Ferris Wheels are built to accelerate fast enough in the correct direction, the result of InGaAs multi-junction (possibly carbonate) high-voltage electricity solar panels with the intense radiation from the sun in space, it alone may override gravity versus centrifugal force opposition strain on SH. The CW will move inward every 12 hours, ±3 hours, during apogee phase of elliptical orbit, or accelerate in the opposite direction during two perogee phases and try to make apogee (semi-major axis) less distant, with a lower eccentricity. This is practical as the Ferris Wheels have an unlimited source of power, but not the H2/O2 fuel rockets. Any CW, coupled with the desire for high mass for, say, 4 ends for 4 armatures of the Ferris wheels, will require many payload trips dragged by elevator or rocket missions, but might be offset with meteorite/asteroid net “capture” and depositing the extraterrestrial material (plentiful on Moon, which can be mined, spacecrafts leave with low escape velocity back to CW) in nets at the ends of the armatures. The Moon has a much lower escape velocity than Earth, so a semi-permanent Moon station, not that much further from CW than earth such that the need for Earth mining of CW Ferris Wheel weights, as the expensive rocket payloads with 19,000 mph escape velocity is too dangerous, expensive, and time consuming, making the extra time to go from CW to Moon and back worth it (the Moon is 320,000 miles away).

All suns eventually explode, like our own, in what’s called a “supernova”.

It will be necessary to leave the solar system someday as the sun is producing too many neutrinos and will eventually explode. Changing climate and weather patterns, and sunspot increase with the other 7 planets getting warmer, means there is a need for a lot more satellites for high-resolution Doppler to better predict weather patterns well in advance, detect incoming asteroids and remote earth-like planets, prevent bottlenecks with cable TV/Internet/cell phone services, useful in the many remote rural areas where terrestrial repeaters are too expensive and take too long to build, without all the regulations and politics, facilitate better navigation for mapping roads, making all cars and other transport vehicles remote controlled for safer and faster service (high resolution for critical mass, or volume times density of vehicles achieved with satellite network, so defiance by terrestrial cell phone repeater firms that will not unite to share bandwidth from greed will be overcome) now find missing people and fugitives optically, with radar, low-light-high-sensitivity, and infrared, assist those with health needs, victims of natural disasters, etc.

With evidence for the Woodward/Mach “Stargate” Effect, traveling at near-relativistic speeds should be possible, taking advantage of internal non-propellant spacecraft as with the man-made flying saucers experienced by Bob Lazar in 1989 with gravity waves produced by heavy elements (Moscovium). Some propellant ejection from not only H2/O2 but U-235, for linear travel and circular oscillation to capitalize on Bernoulli air foil effect in atmosphere, moment of inertia and Woodward/Mach Effect, preferably near heavy objects like Jupiter, the sun, and man-made dual micro-singularities can catapult humans at relativistic (> c for reverse time-travel?) speeds, for journeys to distant planets in what will seem like a short period of time because of Lorentz time dilation. Even without planets, nuclear power along with Stanley Kuprick’s “Ferris Wheels” to simulate gravity, as weightlessness is never good for the body long term, will make it possible to live in areas outside the earth’s atmosphere and outside the solar system after the supernova.

To capitalize on my other inventions, ending all spam (e-mail, Web page, etc.) with power-to-the-consumers regex and GUI acceptance or rejection of not only keywords but number ranges for prices and MLM commissions, see here, extremely critical, as those who are new to our debut can be very-high up a pyramid that sustains itself for life, potential insane wealth, as 35% of gross goes to those who earn referrals through the News Letter down-line.

Thank you for your participation. There is a universe of opportunities for all of us. Please sign-up for our newsletter to stay abreast of earth-shaking developments as I expand our weighted-average industrial democracy and seek out joint venture capitalists for what should cost much less than the proposed $500 billion to make our dreams come true much sooner, safer, and more quickly.



James Dante Wood

Physicist, computer scientist, sole proprietor of SpaceHose.com