• 1580-1600: Sunspot cycle shut down, then solar output fell 0.25%
  
  • “Maunder minimum” (astronomers’ name) aka “the Little Ice Age” (historians’ name)
    
  • Sunspots counted by Galileo Galilei
    
  • Thames River froze over for first time in recorded history
    
  • European population growth stalled
    
  • Crops failed over most of Europe
    
  • Iceland cut off from Europe by sea ice
    
  • Tycho Brahe (Kepler’s mentor) recorded winter temperatures 2.7°F below average
    

• Realize that IPCC’s lower limit (in 3rd Report; 4th is worse) of estimated Greenhouse temperature change is also 2.7°F, but in the opposite direction, so wouldn’t it be neat if...?
  

• Problem: Climate change due to global warming is too fast for human institutions.
  Answer? Slow it down - stop some photons.
  

• Problem: Satellites won’t stay put due to Kepler’s 3^rd Law, infinite fuel requirement, unstable stations.
  Answer? Use reflected sunlight for fuel - steer with it.
  

• Problem: thousands of uncatalogued 300-m class near-Earth objects cruising 'round the 'hood; asteroid-generated tsunami most likely frequent threat.
  Answer? Find the rocks, tag 'em, move 'em, use 'em for construction material.

• Problem: Not enough energy, money, time for the human race to adapt to rapid change.
  Answer? Sell the captured sunlight for power, avoid the insurance hit, maybe even a major war.
  

• Too many eggs in this Terran basket!
  Answer? Move up and out.
  

• scalable (twice the mirror yields twice the cooling)
  
• uncoupled (sails work independently of others)
  
• incremental (pay-as-you-go)
  
• customizable (selectively permeable shields to tailor light or filter out wavelengths?)
  
• minimally intrusive (an array of space mirrors would look like symmetric sunspots)
  
• and above all, reversible (reflectors can easily be shifted to let sunshine through again). All elegant ladies should have a parasol; so should Mother Earth!
  

• Recent cost of climate-related insurance claims & gov't subsidies above background noise: $25 billion/yr
  
  • Typically less than half the actual damage is covered
    
• US GDP, 1999: ~$7 trillion (22% of world total)
  
• Global product, 1999: ~$32 trillion
  
• Recent global insurance load as fraction of GP: ~0.1%
  
• Long-term real product-dot since WW2: 2-¹/₄% (Rule of 72)
  
• Projected real global product, 2100: ~$290 trillion
  
• Cumulative real global product, 2001-2100: ~$12,000 trillion
  
• Forecast global insurance load as fraction of GP, 2100: ~1%
  
  • weather is intensifying, disasters increasing in frequency and amplitude
    
  • more and more people moving to more exposed, marginal lands
    
  • more tightly coupled integrated global society transmits damage signals better
    
  • the more people there are, the more any given material thing is worth
    
• Sum forecasted climate-related hits @ 0.1-1.0% ramp-up: ~$85 trillion ÷ 50% = $170 trillion!
  

• Long term average pop.-dot (population growth) in XX cent.: ~1-¹/₃%
  
  • Note: peaked at ›2% in 1970
• Long term energy-dot since WW2: ~2-¹/₂%
  
• Long term electricity-dot since WW2: ~3-¹/₃%
  

• Conclusions:
  
  • Over time and maturing economy, people use more energy per capita (even though energy per unit output may decrease)
    
  • Electric energy is an increasing fraction of total,
    
  • Also, maybe not strict cause & effect relationship but ample electricity is in fact highly correlated with standard of living and social stability
    

---

• Present U.S. use: 98 quadrillion Btu (1 Btu ~ 1kJ)
  
  • of which 14 quads is electricity
    
• Present global consumption: 353 quads
  
  • of which 58 quads is electricity
    
• Worldwide electrical generating plant, 1995: 2.9 TW
  
• Projected requirement for generating capacity, 2050: ~18 TW
  
• Est. cost of replacement/new generating capacity by 2050 @ $1/watt: ~$18 trillion
  
  • must pay for it twice by 2100 @ 50-year economic life, plus new construction continued growth in demand, so really $110 trillion by 2100
    

• Est. global consumption by 2050: ~1200 quads
  
• Est. electrical demand by 2050: ~300 quads*
  

---

Economic Drivers III

• Create trade in carbon credits?
  
• Human behavior is the last thing to change; what’s the pol/econ value in avoiding that?
  
• What’s the economic value of preserving your way of life?
  
• Cost of climate-related / resource war: who knows? Practically speaking, it’s infinite.
  

---

Another coincidence way too convenient to ignore...

• Given: solar constant @ L1: 1400 W/m² (all waves)
  
• [projected cross sectional area] π (6383 km)² × 0.25% shading ÷ 125% solar limb darkening factor ÷ 82% penumbral shading efficiency = 300,000 km², @ 30-60 grams per square meter, yields sunshade mass ~10-20 million tonnes
  
  • (note: would be 900,000 km² if Parasol Power located further inside at MacInnes Minimum 2.36 Gm)
• 24/7/365 duty cycle
  
• 10% of interdicted sunlight captured
  
• 30% photovoltaic conversion efficiency
  
  • but 72% efficiency may be possible (wow!)
    
  • compare to 38% Carnot efficiency of thermal power cycles
    
• 80% transport efficiency via phased masers, then...

• 1400 MW/km² × 24/7/365 × 300,000 km² × 0.10 × 0.25 × 0.80 ÷ 1055 [J/Btu] = ?
  300 quadrillion British thermal units (Btu), or
  300+ quads!
  same as projected mid-century demand for electricity!

---

Other Grand Constructions
(all CoM figures in 1990$, US)

• Great Pyramid at Giza (Egypt), 2900 BCE: $?? billion
  
• Great Wall (China), 221 BCE-XIV c.: $?? billion
  
• Grand Canal (China), VI-XII c.: $?? billion
• Panama Canal (France, USA), 1878-1894?, 1904-1914: $10? billion
  
• Hoover Dam (USA), 1931-1936: $2? billion
  
• Manhattan Project (USA), 1941-1945: $20? billion
  
• Apollo Project (USA), 1961-1972: $120 billion
  
• Interstate Highway System (USA), 1955-1990: $200 billion
  
• Cold War nuke complex (USA), 1946-1991: $1-5 trillion
  
• Milstar (USA), 1977-2005: $41 billion
  
• SOSUS net (USA), 1980s: $17 billion
  
• International Space Station (int'l), 1983-2010: $95 billion
  
• Three Gorges Dam (China), 1990-2010: $?? billion
  

• Parasols to ameliorate climate change aren’t a cost center, they’re a profit center!
  
• Don’t impose new expenses, simply redirect existing/expected $100T in cash flows
  

• Geostationary orbit is too valuable for other things (e.g. comsats)
  
• Parasol must always remain in line of sight to do any good
  
• Mustn’t disrupt baseline grid
  
• Don’t want to spend a fortune forever on fuel
  

• ...so where?
  
  The L1 region obviously!

• Gravitational fields are conservative;
  
• Natural satellites fall along equipotential lines;
  
• No change in sum (KE+PE);
  
• Action (KE-PE) is minimized.
  
• Behavior is so ingrained we don’t think about it
  

• But think again...
  

Characteristics of Non-Keplerian Orbits


[show Robert Forward’s Statite™ diagram]

• Objects are under continuous acceleration
  
• Also known as radiation-levitated orbits
  
• Can fly arbitrary paths, shapes, trajectories
  
• Patchable!
  

• Trouble is accelerating forever would require infinite fuel according to Rocket Equation...
  

• ...so don’t use rockets!, use the stopped light!
  

Lagrangian Points I


[show general Lagrange diagram]

• At least five points exist for every pair of masses; entire set revolves in phase with the smaller mass
  
• Well defined for Primary >> Satellite (~100:1 mass ratio or better)
  
• Due to shape of space-time at L-points, satellites near them behave as if they’re in orbit around point masses
  
• Collinear case (three unstable (libration) points on line thru Primary-Satellite) discovered in 1767 by Swiss mathematician Leonhard Euler
  
• Triangular case (two stable equilibrium or “Trojan” points, 60° leading (L4) and trailing (L5) satellite) discovered in 1772 by French mathematician Joseph Louis, comte de Lagrange (1736-1813)
  

Lagrangian Points II


[show penumbral shading diagram]

• Sun-Earth system:
  
• S-E L1 is between pair; ~1.5 million km from Earth on axis; always lit; SOHO there already
  
• permissible “halo orbits” inside ellipsoid about 200,000 km (along solar r coord) × 800,000 km (along solar theta coord) × 200,000 km (along solar z coord) centered @ L1; always in light; NASA’s Genesis dwelled there for 6 months
  
• compare S-E L2, ~1.5 million km beyond mass pair; always in shadow; infrared NGST will live there
  
• compare Sun-Earth L3 on far side of Sun; perturbed by other planets more than Earth; totally unstable
  
• compare Sun-Earth L4 & L5; also perturbed by other planets exceeding Earth's effect
  

• Earth-Moon system:
  
• Earth-Moon L1 aka “parking orbit” is ~40,000 km towards Earth on axis
  
• Earth-Moon L4 & L5 are truly stable, deep enough in Terran gravity well for restoring force
  
• Kidney-shaped (limaçon?) halo orbit
  
• L4 & L5 are rare particular solutions of general 3-body problem with M₃ very small:
  
  • See http://www.spof.gsfc.nasa.gov/stargaze/Slagrng3.htm for general proof
    

• Other systems:
  
• Jupiter is big enough, unlike Earth, that it’s trojan points collect debris & eponymous asteroids in long period orbits;
  
• one set (trailing) is named for Trojan heroes, ;
  the other (leading, and separated of course) for the Greek ones (they won the Trojan war)!
  for example, 588 ACHILLES
  

• newly discovered trojan points leading and trailing Neptune with stability zones of huge extent (~1 billion km) containing large moon-size bodies out where the space-time geodesic is flatter
  
• Plus there’s chaos! (orbital resonance or orbital hopping; see the AsiaSat-3A rescue story) which facilitates transitions among orbits if you have the time
  

• Remote master control is not feasible -- round trip = 10 seconds
  
• At speed of sound in material, mechanical time lag in 1000 km structure is tens of seconds (would violate causality otherwise)
  
• Large sail mass(es) on order of 10-100 million tonnes depending on location
  
• Natural frequency is kilosecs or more
  
• Without medium to absorb energy, damping constant is negligible, so must either wait megaseconds or actively damp
  
• Could try more & smaller sails instead, but control problem expands geometrically with number of elements
  
• Massively distributed control architectures may require AI techniques
  

• Moore’s Law, based on decreasing feature size, doesn’t work well in space -- bit-flips, logic gate killed by single hit
  
• Rad-hard electronics must tolerate 5-10 kilorads/year for decades; redundancy/self-repair needed
  
• Solution? Optical processors very fast, very rad-hard, friendly to non-Von architecture (candidates for strong AI maybe?)
  

• Halo orbit about Sun-Earth L1 point (and also L2) subject to periodic (28 day) significant gravitational disturbance (Luna) at just 1/4 distance inside
  

• Keeping a powerful maser(s) trained on a moving target(s) from a moving platform(s) 10 light-seconds (1 million miles each way) away without brownouts or need for customers to apply #2,000,000 sunblock
  

• scalable (twice the mirror yields twice the cooling)
  
• uncoupled (sails work independently of others)
  
• incremental (pay-as-you-go)
  
• customizable (selectively permeable to filter or tailor wavelengths?)
  
• minimally intrusive (an array of space mirrors would look like symmetric sunspots)
  
• and above all, reversible (reflectors can easily be shifted to let sunshine through again).
  

• Herman Kahn:
  
  • "We are now few, poor, and weak; later we will be many, rich, and powerful."
    

• Despite Kahn’s optimism, there may only be a century or two left in this Renaissance culture; all the cheap, easy-to-get fuel, ores, resources are gone; need a functioning technical civilization for Kahn’s Law of Infinite Fungibility to work.
  

• Sagan v. Proxmire debate:
  
  • Sen. WP: “We don’t need to go into space and explore the planets now; the planets will always be there.”
    
  • Dr. CS: “...indeed true, but with an attitude like that, we probably would not.”
    

• Play Dyson Dots™ movie: choose Real Media Player or Windows Media Player
  

• Yes, before moving asteroids around, manipulating terawatt-class directed energy devices, or disseminating self-replicating robots, the human race had better solve the problem of war first.
  

• Until then, send up only most trusted vetted personnel - kosmos not for hoi polloi yet
  

• No, maser energy does not add significantly to heat burden - natural sunlight dumps a gigawattt per km² on ground, so 10 terawatts of power into grid equals a mere 60 mile x 60 mile rectenna @ 1 sol; factoring in waste heat/CO₂ of ground-based carbon-burners, result is huge net heat reduction
  

• Yes, the “halo” orbit nomenclature is indeed duplicative and confusing. Gotta work on that.
  

• Yes, photovoltaic films are far denser than solar sail material, but power generation portion at the hub doesn’t have to be lightweight. In fact, ~100 Mt mass necessary for stability sunward of L1.
  

• No, selling power from space would not violate anticommercial terms of the Outer Space Treaty (which the U.S. hasn't ratified anyway), because the sails are manufactured objects, albeit very large ones made of celestial materials, and not natural celestial bodies.
  

Robert G. Kennedy III, PE is president of the Ultimax Group Inc., a corporation distributed across 11 time zones from Moscow to L.A. He speaks enough languages to start bar fights in all of them. Robotics engineer, amateur historian, and jack of all trades, he spent 1994 working for the House Science Committee’s Subcommittee on Space as ASME’s Congressional Fellow. On the Sputnik anniversary in October 1997, he managed to make the Russian evening news. Robert telecommutes from Oak Ridge, Tennessee, where he resides with his wife, numerous cats, the occasional horse, and a yard full of trees and Detroit iron.

Kenneth I. Roy, PE is an engineer working in Oak Ridge amidst relics of the Manhattan Project. Most of his writing concerns how space technology will affect the future. Notably, “Ship Killers from Space”, a cover story of the prestigious Proceedings of the US Naval Institute, developed the strategic implications of basing kinetic energy weapons in low earth orbit.

I thank my co-authors Ken Roy PE and Dave Fields Ph.D., as well as Anton Smirnov, John Wharton, Eric Hughes, Dwayne A. Day Ph.D., Mike Markowitz, Steven McCauley, Ph.D., and B. Derk Bruins Ph.D. All mistakes are my responsibility.
Particular kudos to:
Anton Smirnov for superb computer artistry.
Mark Seiden for the cute title.
Bill Howe for this excellent CAD rendering of a sunflower-type sail.
Bruce Sterling for the alliterative phrase.
Ken Malpass for this pun.
D. R. Fudge of the ORION stargazing group for pointing out this excellent, and traditionally Southern, acronym.
Dave Fields for coining the Dyson Dot™ nickname.
Marianne Mueller and the AMW Committee for moral and logistical support.
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Update/Event Log

15Feb2001; post original as presented to STAIF 2001
15Feb2001; covered on ABC Evening News
20Feb2001; replace Table 1 with Tables 1-3.
23Feb2001; upload figures and equations.
25April2001; presentation of "AntiVenuforming Terra" at 27th Asilomar Microcomputer Workshop.
24May2001; update figures in Tables 1-3 to reflect limb darkening, L1 stationing.
07Jul2001: "Mirrors & Smoke" appears in Whole Earth Review.
24Sep2001: Finish computer graphic animation of "Mirrors & Smoke" for Belgian national television RTBF - Mati?ére Grise (in English, ’Grey Matter“. Low-rezz version of CG video archived here.
02Nov2001: Deliver invited physics seminar "Mirrors & Smoke: Changing the Solar Constant to a Solar Variable" at California Polytechnic State University, Pomona.
14Nov2001: Deliver invited engineering seminar "Mirrors & Smoke, and Other Shady Schemes" at Stanford University Computer Systems Laboratory Colloquium (EE380).
21Nov2001: Deliver luncheon lecture with updated economic forecasts to Friends of Oak Ridge National Laboratory.
30Jan2007: Advise ABC News Good Morning America re technical background and graphic to illustrate mirrors-in-space concept: © American Broadcasting Company. Note: Not to scale.

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