[ExI] Obama Transition Team Examining Space Solar Power
Kevin H
kevin.l.holmes at gmail.com
Mon Dec 22 17:33:22 UTC 2008
On Sun, Dec 21, 2008 at 5:53 PM, Keith Henson <hkeithhenson at gmail.com>wrote:
>
> it largely depends on the cost to lift power sat parts to GEO.
http://www.spacex.com/falcon9_heavy.php#pricing_and_performance
It's probably the most realistic near-term method, unless we're looking to
NASA, ESA, etc. Looking at the numbers, if we can somehow do this from a
lower orbit it would be much cheaper. I know a low earth orbit would have
some of the same disadvantages as on earth: only twelve hours of sunshine a
day. Someone mentioned a sun-synchronized orbit, but I don't see how that
is possible. The satellite would have to orbit the earth once every year,
which would be way to slow and, to my knowledge, much higher than GEO. But
it seems that full GEO isn't necessary, we could tolerate a couple hours of
night every day, and the costs savings would probably add up when you're
doing this on a large scale.
> The
> advantages are not just in the power multiple, but in the fact that
> the energy is steady, no clouds, no wind stopping, i.e. no storage.
> The other advantage is that you don't have to build massive and very
> expensive lines from the southwest to the mid west and east. You just
> plunk a rectenna down close to the load.
I guess I just don't have a rubric to compare costs here. But yeah, storage
is a big problem here on earth. The other issue, I think, is how *light*
they can make the SPS's. Some of the proposals I've seen (sorry, I can't
find the links right now) don't use solar powers at all, but mirrors to some
device that directly turns visible light radiation into microwaves.
But the solar constant is on average 1366 W/square meter. There's just no
more energy out there from the sun than that at the distance of the Earth (1
AU). That's our upper bound of what we could expect. That's 732 square m
of panels/reflectors to transmit 1GW.
>
>
> If you can haul the parts up on a space elevator, there is no question
> that power sats are the less expensive approach. If you have to haul
> the parts up on rockets, it's marginal.
I think that's the show-shopper here. Rocket technology is here and now. I
think even if we could build a space elevator, even a partial one, it would
take too long to build the technology. Honestly, to save us from the energy
crisis, I think at least part of the system needs to be up and transmitting
power within twenty years, and even that might be stretching it. Some
experts believe that we've already reached peak oil.
> The hybrid methods of using
> rockets to suborbital and lasers to kick the payload into GEO meets
> the penny a kWh requirement.
Except, you know NASA, it would take twenty years to research laser
propulsion before they can approve writing a report on it.
> Of course the old method of developing
> extraterrestrial materials works best of all, but there is not enough
> time to develop space industry.
Has anyone considered pumping hydrocarbons, methane and ethane, from Titan?
We know the lakes are there, the trouble is it would take a long time for
us to get anything back from it. The advantages are that Titan has a
smaller gravity well than the Moon, and the interplanetary transport network
could cause it to cost nearly nothing to transport fuel ships there and
back. Of course, we haven't solved the problem of cost to orbit....
> It's not entirely obvious that any
> long term energy solution is needed. If I were confident the
> singularly would get here before famines and resource wars I wouldn't
> worry about it. But I can't put a firm date on either. The
> consequences of running out of energy are really dire. Some models
> show the population dropping a hundred million a year, bottoming out
> at 1-2 billion.
>
> Keith
I know. This is stuff we should have been working on since the 70's, but
instead forward their problems into the future. BTW, I'm not confident that
a singularity will ever happen.
Kevin
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