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- Path: sparky!uunet!usc!sol.ctr.columbia.edu!emory!rsiatl!ke4zv!gary
- From: gary@ke4zv.uucp (Gary Coffman)
- Newsgroups: sci.space
- Subject: Re: SPS feasibility (WAS: SPS fouling astronomy)
- Message-ID: <1992Aug15.151108.14455@ke4zv.uucp>
- Date: 15 Aug 92 15:11:08 GMT
- References: <1992Aug10.004625.23290@dartvax.dartmouth.edu> <10AUG199219061012@judy.uh.edu> <1992Aug13.075037.2707@ke4zv.uucp> <Bsxo2q.MJy@fmsrl7.srl.ford.com>
- Reply-To: gary@ke4zv.UUCP (Gary Coffman)
- Organization: Gannett Technologies Group
- Lines: 132
-
- In article <Bsxo2q.MJy@fmsrl7.srl.ford.com> wreck@fmsrl7.srl.ford.com (R. Cage) writes:
- >In <1992Aug13.075037.2707@ke4zv.uucp> gary@ke4zv.UUCP (Gary Coffman) writes:
- [deleted]
- >
- >Also, you have the earth's energy budget wrong. The disc area
- >is about pi * (6.4e6 m)^2, or 1.28e14 square meters. The solar
- >constant is about 1360 W/m^2, so we get about 1.75e17 watts, or
- >175,000 TW of incident sunlight. Not 140 TW. You're off by 3
- >orders of magnitude!
-
- Yeah I know. :-( I calculated in English units for Earth's area and
- screwed up the conversion to square meters. Heat load isn't a significant
- factor in any event, even with my wrong numbers it's still piddling.
-
- >Adding another 4 TW of heat is literally a drop in the bucket.
- >Spread it out and you'll have a very hard time detecting it.
-
- Yep.
-
- >>By contrast, for Earth based solar collection, there is no net increase
- >>in heat flux. The energy is striking the planet anyway whether we use it
- >>or not.
- >
- >3.) You're assuming that the albedo of the earth's surface and
- > a solar collector are the same.
- >
- >In a word, WRONG! Solar collectors are a lot blacker than most things.
- >
- >If you counter that the collectors can be interspersed with light
- >colored areas to reflect light and keep the balance the same, you
- >can do that without solar collectors too. It's not an argument
- >for ground-based.
-
- No, all energy that reaches Earth's surface is eventually re-radiated
- to space. The time scale is different if it is immediately reflected
- rather than being used as electricity first, but that doesn't matter
- to the long term energy balance. It's still a piddling amount as you
- noted above.
-
- >>Now what's happening on the Moon? Gas lasers are very inefficient devices.
- >
- >Free-electron lasers aren't. Neither are amplitrons.
- >
- >>I don't have CO2 numbers at hand, but He-Ne efficiencies are around 0.1%.
- >
- >I believe CO2 lasers have reached 20%; someone please correct me.
- >
- >>Now solar energy striking the top of the Earth's atmosphere, or
- >>the surface of the Moon, is 1 kW/m^2.
- >
- >Close enough.
-
- Yeah it's 1.4 but round numbers are close enough for this calculation.
-
- >>So our 1 TW delivered to the busbar on
- >>Earth requires a solar collector area of 1E14 square meters on the Moon.
- >
- >This assumes a system efficiency of 1%. That is about 10x too low. Solar
- >cells are over 20%, conversion equipment to microwaves is well over 50%.
-
- Actually that's an efficiency of 6% total from Lunar solar capture to
- Earth busbar. The figure includes Lunar photovoltaics or thermal at
- roughly 30% efficiency and CO2 lasers at 10%. It doesn't include any
- transmission or conversion losses at either end. The number could be
- 2X either way and still be reasonably close. Since this is the Loony
- Laser we're debunking, microwaves don't count.
-
- >>requires a square 10,000 km on a side, or about 6,000 miles on a side. Sorry
- >>gentlemen, the Moon isn't that big.
- >
- >More like 3,000 km on a side. Just about the area of Luna.
-
- Numbers could be 2X either way. That's still a near *planetary* body
- we're talking about plating with solar cells in any case. That's so
- unreal I'm surprised *anyone* would seriously consider it.
-
- >>Now if we discard the laser, the Moonbase
- >>with it's 6000 mile on a side collector, and simply use the same collector
- >>field we were going to use for the laser on Earth, we still gather in 1E10
- >>watts, or 10 GW, and we haven't spent an improbable fortune on the Moon.
- >
- >You can't use the same collector. It's out of the sun a lot more than
- >half the time, has to be built to deal with WATER and WIND, and a whole
- >lot of other things that limit its life and output. Vacuum and low G
- >has the advantage that it's very friendly to most equipment.
-
- No, it *is* the same collector. The one on Earth to catch the *laser*
- beam from the Moon. It's already built to deal with the elements. It's
- only 6 miles on a side.
-
- >>A Lunar collector array would be in darkness 2 weeks out of 4, so storage
- >>for two weeks would be required on Earth.
- >
- >Wrong. You'd put collectors on both sides of the moon. When power
- >is only hitting the far side, it's the far side collectors which feed
- >the transmitters. Transmission lines are easy in 1/6 G and vacuum.
-
- Plate the *whole* Moon? Really now. Transmission lines would have to
- be superconductive in any case at the power levels we're talking about.
- 1/6 G doesn't really enter in, the damn things would have to be buried
- below the solidly plated surface. Vacuum could be useful for the cryogenics.
-
- >>Therefore, at least half of
- >>Earth's capture arrays would be in daylight at any given moment. That's
- >>at least 7 times better than the Loony Laser.
- >
- >Wrong. Receivers not in direct view of Luna could be fed by
- >reflectors (easy for lasers, a little harder for microwaves).
- >If a receiver can take a feed from more than one reflector at
- >a time, then interruptions from the reflector going behind
- >Earth as seen from Luna will be avoidable.
-
- Ok, now you're going to orbit huge reflectors as well as plate the
- Moon with solar cells. Note that reflectors capable of handling
- terawatts are tricky beasts at best.
-
- >>But solar *thermal* is workable *today* in certain cases.
- >
- >Yes, mostly peaking power or fossil displacement. Not replacement,
- >not base-load. The whole point of Lunetta or SPS is base-load power.
- >
- >IMHO, if there is the capability to build that much collector
- >area on the moon, a single catapult can put it into orbit and
- >leave it in sunlight 24 hours per day, all month. Having many
- >feed angles and immunity from lunar eclipses and beam
- >occultation by Earth is another big advantage. This is why I
- >think SPS has a better future than Lunetta.
-
- A few fast breeders deal with the problem with *today's* technology
- for *trillions* less. I think that they're *all* loony.
-
- Gary
-