Monday, December 27, 2010

Lunar Space Elevator

I will be studying this concept today.  There's a pdf file that I managed to download from this source.  I got the idea from van Pelt's book, which I wrote about previously.  Van Pelt mentioned Jerome Pearson, who is the one who collaborated in the study that I will be reading today.

The thing that got me interested is the Deep Space Station that I've been writing about- which could be used to deploy the cable that would extend from the station down to the lunar surface.  Once the elevator is operational, matter can be gathered from the lunar surface and aggregated to the anchor point in space (through EML-1) where the station can disengage the newly completed elevator, and install another one elsewhere- perhaps on Mars.

I'll check back in when I finish reading the file.

Update:

Mon., Dec. 27th, 10:00 am approx.

Well, I've finished reading the pdf.  Here's a key extract I obtained from the doc.



The DIRECT concept currently in the works would eliminate the need for ion rockets, I would think.  The tanks could fire themselves up to L1 and be joined together to form the counterweight for the lunar space elevator.  So, my idea concurs with this report, if I am not mistaken.

Update 2: Tue., Dec.28, 2010:

Here's a good idea from that pdf:  collect space junk and use it for mass for the lunar space elevator.  The lunar space elevator needs mass and it would be cheaper to get it from space than launching it from Earth or the Moon.  It can serve the dual purpose of cleaning up all the space junk which is a hazard in itself and converting that hazard into a resource.

Another idea for mass is mine.  By surrounding the ET with aluminum covered with shuttle tiles, the ET can become a fuel depot as well as a mass anchor for a lunar space elevator.  A fully loaded ET can weigh over a million pounds.

If you were to keep all six ET's I proposed together at EML-1, that would be plenty of mass.

Another idea occurred to me: after putting the shuttle tiles down, you could put thin film photovoltaic cells on top of it.  That stuff comes in sheets.  Since it is lightweight and comes in sheets, it should be easy to do this.  You could think of the box surrounding the ET as cold box that keeps stuff very cold inside, but also as a scaffold for solar power that can power the entire station and then some.  These ideas combined together can be said to be synergistic.

Update 3: Tue., Dec. 28, 2010, 7 am. approx.

Looks like there needs to be a lot of mass lifted into space for the counterweight.  Here's the key passage for this from the pdf.  Launch costs of 24 billion.  I wonder: could this be merged with the Moonbase expenditures in order to consolidate costs?  There's overlap in the two propositions, that's why I pose the question.



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