Interesting energy saving technology.The lunar version will probably need cooling radiators.
Not really it's using the sun directly to melt the material.Conduction with the lunar surface and radiation might be enough for the work piece to cool.Scaled up it would be the machine moving vs the work piece which would be sitting on the lunar surface.
I think you're missing the fact that minimal heat loss is a GOOD thing. There is some inevitable heat loss due to radiation and conduction to the rest of the work piece. The higher this heat loss, the greater the amount of power required to maintain the desired sintering temperature. That implies a larger solar concentrator.Conversely, the smaller the heat loss, the smaller the solar concentrator required to produce a working system. This also concentrates the sunlight onto a smaller area, so higher resolution product pieces with thinner walls and finer details are possible.Of course, a smaller solar concentrator with a smaller amount of power will also have a reduced production rate (by product mass). However, the production rate can be increased simply by using more solar concentrators to work on more work pieces. For example, if the required solar concentrator area is reduced by a factor of 4, simply make 4 solar concentrator systems to produce 4 work pieces at the same time.
Due to low shipping weight, mirrors made from ultra light Mylar might be more cost effective than using Fresnel lens, even if Mylar mirrors ended up being less efficient from a energy conversion perspective. Because the Moon is in vacuum, Mylar mirrors can be very light weight (with their shapes sewn on Earth) and mounted on ultra light scaffolding.
Quote from: Bill White on 06/27/2011 02:54 pmDue to low shipping weight, mirrors made from ultra light Mylar might be more cost effective than using Fresnel lens, even if Mylar mirrors ended up being less efficient from a energy conversion perspective. Because the Moon is in vacuum, Mylar mirrors can be very light weight (with their shapes sewn on Earth) and mounted on ultra light scaffolding.Would the mylar mirrors be vulnerable to the abrasive lunar dust?
However, it appears that ū mil Mylar film is about 20 gm/m^2 and with added layers of underside backing can come in at about 210 gm/m^2
Therefore, 1 kilogram of material could provide about 5 square meters of Mylar mirror, right?
But lets add margin and go with 1 kg per square meter of Mylar mirror (excluding support frames, etc . . . )Deliver 2000 kg worth of Mylar fabric to the lunar surface and you will have 2000 square meters of mirrored surface available to deploy or 1.25 square miles of mirrored surface, right?